EP1581752A2 - Flexible flywheel for torque transmission device - Google Patents

Flexible flywheel for torque transmission device

Info

Publication number
EP1581752A2
EP1581752A2 EP04700270A EP04700270A EP1581752A2 EP 1581752 A2 EP1581752 A2 EP 1581752A2 EP 04700270 A EP04700270 A EP 04700270A EP 04700270 A EP04700270 A EP 04700270A EP 1581752 A2 EP1581752 A2 EP 1581752A2
Authority
EP
European Patent Office
Prior art keywords
steering wheel
axis
wheel according
radial arms
oscillation
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP04700270A
Other languages
German (de)
French (fr)
Inventor
Roel Verhoog
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Valeo Embrayages SAS
Original Assignee
Valeo Embrayages SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Valeo Embrayages SAS filed Critical Valeo Embrayages SAS
Publication of EP1581752A2 publication Critical patent/EP1581752A2/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D3/00Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
    • F16D3/50Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members
    • F16D3/60Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members comprising pushing or pulling links attached to both parts
    • 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
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D13/00Friction clutches
    • F16D13/58Details
    • F16D13/70Pressure members, e.g. pressure plates, for clutch-plates or lamellae; Guiding arrangements for pressure members
    • 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
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D3/00Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
    • F16D3/50Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members
    • F16D3/78Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members shaped as an elastic disc or flat ring, arranged perpendicular to the axis of the coupling parts, different sets of spots of the disc or ring being attached to each coupling part, e.g. Hardy couplings
    • F16D3/79Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members shaped as an elastic disc or flat ring, arranged perpendicular to the axis of the coupling parts, different sets of spots of the disc or ring being attached to each coupling part, e.g. Hardy couplings the disc or ring being metallic
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/10Suppression of vibrations in rotating systems by making use of members moving with the system
    • F16F15/12Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon
    • F16F15/1201Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon for damping of axial or radial, i.e. non-torsional vibrations
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/10Suppression of vibrations in rotating systems by making use of members moving with the system
    • F16F15/12Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon
    • F16F15/131Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon the rotating system comprising two or more gyratory masses
    • F16F15/13107Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon the rotating system comprising two or more gyratory masses for damping of axial or radial, i.e. non-torsional vibrations
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/10Suppression of vibrations in rotating systems by making use of members moving with the system
    • F16F15/12Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon
    • F16F15/131Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon the rotating system comprising two or more gyratory masses
    • F16F15/13142Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon the rotating system comprising two or more gyratory masses characterised by the method of assembly, production or treatment
    • F16F15/1315Multi-part primary or secondary masses, e.g. assembled from pieces of sheet steel
    • 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
    • F16F15/30Flywheels
    • 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
    • F16F15/30Flywheels
    • F16F15/315Flywheels characterised by their supporting arrangement, e.g. mountings, cages, securing inertia member to shaft
    • 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
    • F16F2228/00Functional characteristics, e.g. variability, frequency-dependence
    • F16F2228/06Stiffness

Definitions

  • the invention relates to a flexible flywheel for a torque transmission device, in particular for a motor vehicle, this flexible flywheel being intended to be driven in rotation about an axis by a driving shaft and comprising an annular mass carried by a flexible element intended to be fixed to the driving shaft.
  • the driving shaft is the crankshaft of an internal combustion engine
  • the torque is transmitted to a driven element such as the input shaft of a gearbox for example, generally by means of at least one clutch and a torsional damper.
  • the flywheel is the primary flywheel of a double damper flywheel, which also includes a secondary flywheel centered and guided in rotation on the primary flywheel by means of a bearing, and a damper. torsional mounted generally between the two flywheels, the secondary flywheel forming the clutch reaction plate for transmitting a torque to the input shaft of a transmission.
  • the annular mass of a flexible flywheel is generally formed by a cast iron ring fixed by screws or rivets on the radially external periphery of a flexible annular sheet, the radially internal peripheral part of which comprises fixing screw passage holes on the driving shaft, that is to say on the crankshaft of an internal combustion engine in the case of a torque transmission device for a motor vehicle.
  • the flexible annular sheet has a relatively small thickness (of the order of 2 to 3 mm for example) and its radially internal peripheral part for fixing to the driving shaft is reinforced by a stiffening washer having a greater thickness and on which heads fixing screws can be supported.
  • This thin annular sheet must be checked after cutting, possibly straightened and carefully assembled with the annular mass in cast iron. These operations are relatively long and delicate and are therefore expensive.
  • a flywheel of this type deforms in "pumping" bending (bending deformation in which the flexible flywheel remains substantially parallel to itself) and in oscillation around an axis which is perpendicular to the axis of rotation of the flywheel and which has a determined angular position relative to the crankshaft, this oscillation being linked to a bending of the last crankpin of the crankshaft.
  • Known flexible flywheels are characterized by a structure with symmetry of revolution and are therefore not designed to take this oscillation phenomenon into account.
  • the invention particularly relates to a flexible steering wheel which meets this need and which does not have the drawbacks of the flexible steering wheels of the prior art.
  • a flexible flywheel for a torque transmission device in particular for a motor vehicle, intended to be driven around an axis of rotation by a drive shaft and comprising an annular mass carried by a flexible element intended to be fixed to the driving shaft, characterized in that this flexible element comprises radial arms defining a preferred axis of oscillation perpendicular to the axis of rotation of the flywheel.
  • the flexible flywheel according to the invention is therefore particularly designed to respond to the aforementioned oscillation phenomenon and to absorb it, at least in part, by decoupling from the shaft driving the flywheel oscillating around the preferred axis.
  • the radial arms of the flexible element can advantageously be formed by a local excess thickness of this flexible element.
  • the flexible element has a greater thickness in its parts which form the radial arms, and it has a greater thickness. low in its other parts, this smaller thickness can be reduced and even canceled as soon as the radial arms have a thickness and a rigidity sufficient to ensure the transmission of the torque between the driving shaft and the driven shaft.
  • the flexible element of the flexible steering wheel according to the invention can then be formed from a thicker sheet than in the prior art, which can be of a lower quality and which does not need pretreatment, which is more easy to work, which deforms less and which does not need to be straightened, so that the steering wheel according to the invention is less expensive than in the prior art.
  • the axis of oscillation is formed by two radial arms which extend in line with one another substantially between the axis of rotation and the annular mass of inertia or else three radial arms, two of which are symmetrical to each other with respect to the extension of the third, these three radial arms each extending between the axis of rotation and the annular mass.
  • the flexible element is formed of a disc having symmetrical recesses formed on either side of the axis of oscillation. These recesses can be through or not.
  • the flexible element When the flexible element is not formed in one piece with the annular mass, it is fixed to the latter by screws, rivets or the like, at the ends of the above-mentioned radial arms.
  • the flexible element can be formed either of a single sheet metal element of a desired thickness, or of several flat elements superimposed and fixed together on the annular mass.
  • the flexible flywheel comprising hysteresis means carried by the flexible element and cooperating by friction with the annular mass.
  • these hysteresis means comprise two radial arms extending perpendicular to the axis of oscillation and having radially internal ends integral with the flexible element and radially external ends in contact with the annular mass.
  • the radial arms of the hysteresis means are formed in one piece with the flexible element or, as a variant, are part of a washer attached to the flexible element, this washer being intended to be fixed with the flexible element. on the leading tree.
  • the hysteresis means comprise elastic pins mounted in semi-cylindrical housings with two lugs secured to the flexible element and two lugs secured to the annular mass, these lugs extending in one direction perpendicular to the above-mentioned axis of oscillation.
  • the radial arms which define the axis of oscillation comprise, between their radially internal and radially external ends, cutouts or notches for locating maximum stresses.
  • the aforementioned radial arms may extend perpendicular to the axis of rotation or may be slightly inclined obliquely relative to a perpendicular to the axis of rotation, for example in a direction opposite to the shaft leading from their ends radially internal.
  • the flexible element comprises means defining a second axis of oscillation which is perpendicular to the axis of rotation and to the first axis of oscillation mentioned.
  • the two axes of oscillation are defined by radial arms of the flexible element.
  • these radial arms are connected to the annular mass by tongues which have different stiffnesses depending on whether they connect to the annular mass the radial arms defining the first axis of oscillation or those defining the second axis of oscillation.
  • the flexible flywheel according to the invention can in particular form the primary flywheel of a double damper flywheel which also comprises a secondary flywheel intended to be connected to the input shaft of a transmission by a clutch and a shock absorber of torsion mounted between the two flywheels.
  • the torsion damper is of the type comprising springs oriented radially with respect to the axis of rotation, in the rest position of the double damping flywheel.
  • the hysteresis means associated with the flexible primary flywheel advantageously comprise an elastic washer which is carried by the flexible element of the primary flywheel and which comes to bear on the latter, or else which is mounted between the flexible element of the primary flywheel and the annular mass carried by this flexible element.
  • FIG. 1 is a schematic front view of a flexible steering wheel according to the invention
  • - Figure 2 is a schematic view in axial section of the steering wheel of Figure 1
  • Figures 3 and 4 are views similar to Figures 1 and 2, for an alternative embodiment of the flexible steering wheel
  • Figures 5 and 6 are views similar to Figures 1 and 2 for another alternative embodiment
  • Figure 7 is a schematic view in axial section of another alternative embodiment of the flexible flywheel
  • Figure 8 is a schematic perspective view of the steering wheel of Figure 7
  • - Figures 9 and 10 are views similar to Figures 1 and 2 for another alternative embodiment of the invention
  • FIG. 11 schematically represents an arrangement of consecutive flexible elements in a sheet metal strip before cutting
  • Figure 12 is a schematic elevational view of another alternative embodiment of the flexible flywheel
  • Figure 13 is a schematic perspective view of the steering wheel of Figure 12;
  • Figure 14 is a schematic front view of another alternative embodiment of the flexible steering wheel;
  • Figures 15 and 16 are schematic sectional views along lines XV-XV and XVI-XVI respectively of Figure 14;
  • Figure 17 is a schematic front view of yet another alternative embodiment of the flexible steering wheel
  • Figures 18 and 19 are schematic views in axial section in two perpendicular planes of the steering wheel of Figure 17;
  • Figure 20 is a schematic front view of yet another alternative embodiment of the flexible steering wheel
  • Figure 21 is a partial schematic view in axial section, on a larger scale, of the steering wheel of Figure 20; - Figure 22 is a schematic front view of another alternative embodiment of the flexible steering wheel on the invention;
  • Figure 23 is a schematic view in axial section of a double damping flywheel according to the invention.
  • Figure 24 is a schematic half-view in axial section of an alternative embodiment of the double damping flywheel
  • Figures 25 and 26 are schematic views in axial section of two other alternative embodiments of the double damping flywheel according to the invention.
  • Figure 27 is a schematic view of the steering wheel of Figure 1 describing its positioning relative to the drive shaft.
  • FIGS. 1 and 2 a first embodiment of a flexible flywheel according to the invention is shown diagrammatically.
  • This flexible flywheel is intended for the transmission of a torque between a driving shaft 12 which is the crankshaft of an internal combustion engine of a motor vehicle, and a driven shaft (not shown) which is the input shaft of a gearbox for example, and which is intended to be mounted integral in rotation with a hub 14 of a torsional damper coaxial with the flywheel 10 and the driving shaft 12 .
  • the hub 14 of the torsion damper is, in known manner, connected by a clutch E to the flywheel 10, a radial face 16 oriented on the side opposite to the drive shaft 12 forms a friction surface cooperating with the disc clutch 18 of clutch E.
  • the flywheel 10 is fixed at the end of the driving shaft 12 by screws 20, oriented parallel to the axis 22 of rotation of the shaft 12 and of the flywheel 10, and distributed evenly in circle around this axis 22.
  • the screws 20 are received in orifices 24 of a radially internal annular part 26 of the flywheel 10, this annular part 26 being connected by two radial arms 28 diametrically opposite to an annular mass 30 which surrounds the annular part 26 and whose external cylindrical periphery carries ignition targets 32.
  • annular mass 30 are formed in a single piece of cast steel of a quality resistant to bending stresses, for example in spheroidal graphite cast iron.
  • the arms 28 are not exactly perpendicular to the axis of rotation 22, but are inclined slightly obliquely and extend towards the clutch from the annular part 26. This makes it possible to increase the axial stiffness of the flywheel which resists better with declutching efforts, and increase the pumping frequency.
  • the radial arms 28 have dimensions in width and in thickness which make it possible to transmit the maximum torque generated by the internal combustion engine of the motor vehicle.
  • axis of oscillation 34 which is perpendicular to the axis of rotation 22 and whose angular position around this axis is determined relative to the drive shaft 12 and is known by measurement or by calculation (the position angular of the flywheel 10 relative to the driving shaft 12 being itself fixed and determined for mounting by appropriate means).
  • the annular part 26 and the radial arms 28 of the flywheel define a flexible element, similar to the flexible annular sheet of a flexible flywheel of the prior art, allowing deformations of the flywheel in bending (the annular mass 30 then moving parallel to itself).
  • the radial arms 28 of the flywheel 10 also allow an oscillation of this flywheel about the axis 34, this oscillation being linked to a bending of the last crankpin of the crankshaft forming the driving shaft 12.
  • the section of the radial arms 28 is determined for example to allow this oscillation phenomenon at a vibration frequency of the crankshaft which corresponds to a rotation speed of approximately 2700 to 4500 revolutions per minute.
  • the diameter of the friction is 220 mm
  • the radial arms 28 have a cross section of oblong or substantially rectangular shape with rounded ends
  • the flywheel of inertia is made of spheroidal graphite cast iron having a breaking strength of the order of 500 MPa
  • the radial arms 28 have a thickness of 6 to 10 mm for a width of 30 to 40 mm.
  • the radii of the connections 36 of the radial arms to the annular mass 30 are determined to reduce the stress concentrations and are for example approximately 8 mm.
  • the damping in spheroidal graphite cast iron is approximately three or four times greater than the damping in steel.
  • the axis of oscillation 34 of the flywheel 10 is defined by a radial arm 28 identical to those already described and by two other radial arms 40 which are symmetrical one on the other relative to the axis 34 and which extend in directions substantially opposite to that of the radial arm 28 relative to the axis of rotation 22, these radial arms 40 making an angle of about 140 degrees with the radial arm 28 in the example shown.
  • These two radial arms 40 are a little easier to foundry than a single radial arm 28 and can also reduce the problems of molding shrinkage.
  • the structure of the flywheel 10 shown in FIGS. 3 and 4 is identical to that of the flywheel in FIGS. 1 and 2.
  • the flywheel 10 is of the type shown in FIGS. 1 and 2 and is associated with hysteresis means making it possible to dampen the oscillations of the flywheel around the defined axis 34 by the radial arms 28.
  • hysteresis means comprise an elastic washer 42 of annular shape, made for example of spring steel and intended to be fixed on the end of the aforementioned driving shaft at the same time as the annular part radially internal 26 of the flywheel.
  • the elastic washer 42 has orifices 44 coinciding with the orifices 24 formed in the annular part 26 for the passage of the fixing screws 20, and its internal diameter is substantially equal to that of the annular part 26 of the flywheel.
  • This elastic washer 42 comprises two diametrically opposite radial arms 46, which extend in a direction perpendicular to the axis of oscillation 34 and whose radially external ends 48 are bent parallel to the axis to come to apply pressure on the internal cylindrical surface 50 of the annular mass 30.
  • any oscillation of the annular mass 30 around the axis 34 results in friction on the folded ends 48 of the arms of the elastic washer 42 secured to the radially internal annular part 26 of the flywheel .
  • the ends 48 of the arms 46 extend through small orifices formed in a veil connecting the annular part 26 to the annular mass 30.
  • the flywheel inertia 10 according to the invention is formed of two independent elements which are fixed to each other, namely a flexible element 52 made of sheet steel and an annular mass of inertia 30 made of cast iron, the element flexible 52 being of generally annular shape and being fixed at its radially outer periphery to the mass of inertia 30 by screws 54, rivets or the like.
  • the flexible element 52 comprises a radially internal annular part 56, formed with holes 58 for the passage of the fixing screws on the end of the driving shaft, a radially external annular part 60 comprising holes for the passage of the fixing screws 54 on the annular mass 30, and two radially opposite radial arms 62, which connect the annular parts 56 and 60 together.
  • the flexible element 52 is formed of an annular washer in which two diametrically opposed cutouts 64 are formed, substantially in the shape of a bean, which define between them the radial arms 62.
  • the flexible element 52 is formed from a steel sheet which has a thickness considerably greater than that of the steel sheets forming the flexible elements of the flexible flywheels of the prior art, this thickness being for example of around 5 mm. This thickness reduces the risks of deformation of the sheet during its machining and facilitates and simplifies the manufacture of the flexible element 52.
  • the axis of oscillation of the flywheel is defined by the diametrical axis of symmetry of the radial arms 62.
  • the flexible element 72 of the flywheel 10 is essentially formed by an internal annular part 74 which includes the orifices 76 for the passage of the fixing screws on the end of the driving shaft, of two radial arms 78 of the aforementioned type which define the axis of oscillation of the flywheel and which have radial extensions 80 towards the outside, these extensions 80 forming fixing zones on the annular mass 30 and comprising for this purpose holes for fixing screw 82, rivets or the like.
  • Notches or cutouts 84 are formed in the sides of the radial arms 78, in order to constitute zones for locating maximum stresses and to separate these maximum stresses from the orifices for the passage of screws 82.
  • FIG. 11 schematically represents a succession of flexible elements such as the element 52 of FIGS. 7 and 8, and the outer peripheral edge 86 of which has a notch 88 and a point 90 diametrically opposite, this point and this notch making it possible to nest partially in each other the flexible elements 52 during their formation in a sheet metal strip.
  • the tip 90 of an element 52 extends inside the notch 88 of the next element 52 and so on.
  • the tip 90 of each flexible element 52 is itself formed by two curved notches 92 formed in the radially external annular part 60 of the flexible element.
  • the flexible element of the flywheel 10 according to the invention is of the same type as the flexible element 72 of Figures 9 and 10 and is associated with hysteresis means formed by an elastic element 96 in the shape of a cross, which extends in a plane perpendicular to the axis of rotation and which is applied to the element 72.
  • This elastic element 96 comprises two radially opposite radial arms 98, which have the same forms that the radial arms 78 of the flexible element 72 and which are superimposed on the latter and two other radial arms 100 perpendicular to the radial arms 98 and having a radially external end 102 supported on a radial face of the inertia mass 30 for generate a damping by radial friction during the oscillations of the flywheel around the axis defined by the radial arms 78 and 98.
  • the elastic element 96 is fixed at the ends of its radial arms 98 to the annular mass 30 by the screws 82 for fixing the flexible element 72, and its radially internal annular part includes orifices 104 for passage of the steering wheel fixing screws. of inertia on the leading tree.
  • the flexible element 72 can be formed by a stack of elongated flat elements made of thin sheet, and the elastic element 96 is part of the stack.
  • the flywheel 10 is made in one piece, for example of cast iron, and its radially internal annular part 26 is connected to the annular mass 30 by two radial arms 28 diametrically opposite, similar to those of the embodiment of FIGS. 1 and 2, and by an annular web 108 of relatively small thickness, which occupies the entire space between the annular part 26, the annular mass 30 and the radial arms 28.
  • the flexible element of the steering wheel is then a ring comprising local excess thicknesses forming the radial arms 28.
  • this flywheel has the same structure as that of FIGS. 1 and 2.
  • the flexible flywheel 10 comprises an annular mass 30 in cast iron and a flexible element of the type shown. Figures 9 and 10, this flexible element being formed of a stack of identical elements 72 made of thin sheet.
  • this flexible element is fixed to the annular mass 30 by screws 82, rivets or the like at the ends 80 of its radial arms 78 defining the axis of oscillation.
  • the stack of identical elements 72 is applied to a thin annular sheet 110 fixed to the annular mass 30 by the screws 82 for fixing the flexible elements 72, the periphery of this thin annular sheet 110 being supported on a radial face of the annular mass 30 and thus constituting hysteresis means for damping the flexions and oscillations of the flywheel.
  • the stacked elements 72 can have different thicknesses, greater in the middle of the stack than at its ends, to equalize the bending stresses. The hardnesses of the stacked elements can also be different.
  • the flexible flywheel 10 is made in one piece and comprises a radially internal annular part 26 connected by two radial arms 28 diametrically opposite an annular mass 30, as in the modes of embodiment already described, and further comprises two radial lugs 112 which are oriented perpendicular to the axis of oscillation 34 defined by the radial arms 28, and which extend from the annular part 26 towards the annular mass 30.
  • This this also includes two radial lugs 114, oriented towards the annular part 26 from the internal cylindrical surface of the annular mass 30, the radial lugs 112 and 114 being aligned in pairs and ending in semi-cylindrical housings oriented towards each other and in which are housed means such as elastic pins 116 forming hysteresis means for damping the oscillations of the flywheel around the axis 34.
  • the hysteresis means comprise intermediate elements mounted between the part annular 26 and the annular mass 30, in a direction perpendicular to the axis 34.
  • the flexible flywheel 10 comprises a radially internal annular part formed with orifices 24 for passage of the fixing means on the driving shaft and with four radial arms 28 of the aforementioned type, which are oriented 90 degrees from each other and which are connected at their ends radially ex dull to the annular mass 30 by elastically deformable tongues 120, 122 which extend in a plane perpendicular to the axis of rotation and which are fixed at their ends to the radial arms 28 and to the annular mass 30 by screws, rivets or the like.
  • each tongue 120, 122 is of elongated shape and extends in a direction substantially perpendicular to the radial arm 28 on which it is fixed.
  • Two axes 34, 124 of oscillation of the flexible flywheel are thus defined which are perpendicular to the axis of rotation and perpendicular to each other, one of these axes of oscillation corresponding to the above-mentioned axis 34 and the other 124 itself. being perpendicular.
  • the tongues 120 fixed to the radial arms 28 defining the axis of oscillation 124 have a stiffness less than that of the tongues 122 fixed to the radial arms 28 defining the axis of oscillation 34.
  • the oscillation around the axis 34 is characterized by a low stiffness and therefore by a low frequency, while the oscillation around the axis 124 is characterized by a greater stiffness and therefore by a higher frequency.
  • the same result can be achieved by having different masses generating different inertias on the two oscillation axes 34 and 124.
  • the oscillation frequency is lower around the axis perpendicular to this axis of oscillation. It is of course possible to combine these two means, that is to say to differentiate the stiffnesses of the tongues 120 and 122 and the masses disposed on the axes of oscillation.
  • the flexible flywheel according to the invention forms part of a double damping flywheel and forms the primary flywheel thereof.
  • the flexible primary flywheel 10 comprises a radially internal annular part 26 forming a hub, to which is fixed by rivets 130 the radially internal part of a flexible annular sheet 132 whose radially external periphery is fixed by axial clamping on a annular mass 30 formed of two cylindrical rings 134, 136, welded one inside the other, the external periphery of the annular sheet 132 being clamped between an axial end of the internal ring 134 and an end flange of the outer ring 136.
  • Hysteresis means are associated with this flexible annular sheet and are formed by an elastic washer 138 whose radially outer periphery is clamped with the radially outer periphery of the annular sheet 132 between the rings 134 and 136 as indicated, and whose radially internal annular part comprises radial lugs 140 which are applied elastically to the flexible annular sheet 132.
  • the flexible primary flywheel 10 is associated with a secondary flywheel 142 which is centered and guided in rotation on the hub 26 by means of a plain bearing 144 and which forms the reaction plate of a clutch of a conventional type.
  • a torsional damper 146 with circumferential springs is mounted between the two flywheels and connects them in rotation with a possibility of angular movement between them, for the absorption of vibrations and torque irregularities.
  • This torsional damper conventionally comprises an input element which is integral in rotation with the primary flywheel 10 and an output element which is integral in rotation with the secondary flywheel 142, the input element here being fixed by rivets 148 on the elastic washer 138 while the outlet element is fixed by rivets 150 on the secondary flywheel.
  • a torque limiter is formed by the axially clamped mounting of the external periphery of the annular sheet 132 between the rings 134 and 136 of the annular mass 30, this axial clamping allowing relative rotation of the annular sheet 132 relative to the washer. elastic 138 when the transmitted torque is greater than a predetermined maximum value.
  • the primary flywheel 10 comprises a flexible annular sheet 152 whose radially internal part is fixed by means of screw 154 on the end of the shaft leading at the same time as a cylindrical hub forming the internal annular part 26 of the flexible flywheel, and the radially external annular part of this sheet 152 is fixed by rivets 156 on an annular mass 30 cast.
  • This annular mass 30 carries a starter ring as well as a closing plate 158 on the side opposite to the driving shaft, this plate 158 being fixed to the annular mass 30 by rivets 160 and comprising an internal peripheral rim 162 oriented radially and disposed in the vicinity of the flexible annular sheet 152.
  • An elastic washer 164 is mounted between the flexible annular sheet 152 and the flange 162 of the closure sheet 158 and forms hysteresis means for damping the bending vibrations of the primary flywheel 10.
  • the double damping flywheel shown in axial section comprises a flexible primary flywheel 10 according to the invention, a secondary flywheel 170 formed by two annular parts 172 and 174 connected together by a torque limiter 176, a bearing 178 for centering and guiding in rotation the secondary flywheel 170 on a cylindrical hub formed by the radially internal annular part 26 of the primary flywheel 10, and a torsion damper 180 which is mounted between the two flywheels and which is of the radial or radial spring type.
  • the springs 182 of this torsion damper are guided on cylindrical rods 184 housed in cylindrical boxes 186, which are pivotally mounted at their radially external ends on the annular mass 30 of the primary flywheel around a parallel axis 188 to the axis of rotation, while the radially internal ends of the cylindrical rods 184 are pivotally mounted on the internal annular part 174 of the secondary flywheel 170 by means of axes 190 parallel to the axis of rotation.
  • the annular mass 30 of the primary flywheel comprises blocks 192 of cast iron, housed between the cylindrical boxes 186 of the springs of the torsion damper and having a substantially triangular shape with apex oriented towards the axis of rotation to allow angular movement of the boxes.
  • the masses of the blocks 192 can be distributed on the two perpendicular axes of oscillation 34 and 124, as described with reference to FIG. 22.
  • the blocks 192 are fixed by rivets 194 to a sheet 196 of the annular mass 30 of the primary flywheel, at the same time as the radially external part of the flexible annular sheet 132 of the primary flywheel.
  • An elastic washer 198 is mounted between the annular sheet 132 and a radial flange 200 of the aforementioned sheet 196, on the side of the primary flywheel facing the driving shaft. This elastic washer forms means for damping the flexural vibrations of the primary flywheel.
  • FIG. 26 differs from that of FIG. 25 only by the constitution of the blocks 192 carried by the primary flywheel, which here consist of an axial stack of sheets 202 fixed by the aforesaid rivets 194 on the sheet. 196 of the primary flywheel, at the same time as the radially external peripheral part of the flexible annular sheet 132.
  • the driving shaft 12 is generally a crankshaft comprising at least one crankpin 1200,1201 capable of being connected to at least one connecting rod (not shown) associated with a piston of a heat engine.
  • the crank pin called first crank pin 1200 is adjacent to the flexible flywheel 10 according to the invention.
  • the crankpin 1200 defines in association with the axis of rotation 22 of the driving shaft and the flexible flywheel 10 a plane P.
  • the axis of oscillation 34 of the flexible flywheel 10 according to the invention is substantially perpendicular to the axis of rotation 22 and it is positioned angularly with respect to the driving shaft 12. This angular position is determined between the plane P previously described and the axis of oscillation 34 which then have a positioning angle ⁇ between them.
  • the value of the positioning angle ⁇ is optimized in order to allow a reduction of the stresses in the driving shaft and / or of the noises generated by the motor.
  • the value of the positioning angle ⁇ is determined by measurement or by calculation. This value is a function of the number of cylinders of the thermal engine considered as well as of the arrangement of said cylinders. This value is also a function of the phenomenon or phenomena for which a reduction is sought (essentially the constraints and the noises).
  • the value of the positioning angle ⁇ is measured in a direction of rotation R of the shaft leading from the plane P to the axis of oscillation 34 of the flexible flywheel 10 along the invention.
  • the value of the positioning angle ⁇ can be between approximately 80 ° and approximately 120 °. This makes it possible to weight the reduction in noise generated compared to the reduction in stresses and vice versa.
  • the value of the positioning angle ⁇ can be between approximately 90 ° and around 110 °.
  • the stresses are reduced, while for a value of the positioning angle ⁇ of around 110 °, the noise generated is reduced.
  • the intermediate values of the positioning angle ⁇ make it possible to adapt the stress and noise reductions generated as a function of what is sought in this material.

Abstract

The invention concerns a flexible flywheel for torque transmission device, in particular for a motor vehicle, comprising a radially internal annular element (26) including means for being fixed on an input shaft and linked through at least two diametrically opposite radial arms (28) to an annular mass (30), the radial arms (28) defining an oscillation axis (34) for the flywheel perpendicular to the axis of rotation and which has a predetermined angular position relative to the input shaft.

Description

VOLANT D'INERTIE FLEXIBLE POUR DISPOSITIF DE TRANSMISSION DE COUPLE FLEXIBLE FLYWHEEL FOR TORQUE TRANSMISSION DEVICE
L'invention concerne un volant d'inertie flexible pour dispositif de transmission de couple, en particulier pour véhicule automobile, ce volant flexible étant destiné à être entraîné en rotation autour d'un axe par un arbre menant et comprenant une masse annulaire portée par un élément flexible destiné à être fixé à l'arbre menant.The invention relates to a flexible flywheel for a torque transmission device, in particular for a motor vehicle, this flexible flywheel being intended to be driven in rotation about an axis by a driving shaft and comprising an annular mass carried by a flexible element intended to be fixed to the driving shaft.
Dans le cas d'un dispositif de transmission de couple pour véhicule automobile, l'arbre menant est le vilebrequin d'un moteur à combustion interne, et le couple est transmis à un élément mené tel que l'arbre d'entrée d'une boîte de vitesses par exemple, en général par l'intermédiaire d'au moins un embrayage et un amortisseur de torsion.In the case of a torque transmission device for a motor vehicle, the driving shaft is the crankshaft of an internal combustion engine, and the torque is transmitted to a driven element such as the input shaft of a gearbox for example, generally by means of at least one clutch and a torsional damper.
Dans certaines réalisations, le volant d'inertie est le volant primaire d'un double volant amortisseur, qui comprend également un volant d'inertie secondaire centré et guidé en rotation sur le volant primaire par l'intermédiaire d'un palier, et un amortisseur de torsion monté en général entre les deux volants d'inertie, le volant secondaire formant le plateau de réaction de l'embrayage pour la transmission d'un couple à l'arbre d'entrée d'une transmission.In certain embodiments, the flywheel is the primary flywheel of a double damper flywheel, which also includes a secondary flywheel centered and guided in rotation on the primary flywheel by means of a bearing, and a damper. torsional mounted generally between the two flywheels, the secondary flywheel forming the clutch reaction plate for transmitting a torque to the input shaft of a transmission.
Dans la technique actuelle, la masse annulaire d'un volant d'inertie flexible est en général formée par une couronne en fonte fixée par des vis ou des rivets sur la périphérie radialement externe d'une tôle annulaire flexible dont la partie périphérique radialement interne comporte des trous de passage de vis de fixation sur l'arbre menant, c'est à dire sur le vilebrequin d'un moteur à combustion interne dans le cas d'un dispositif de transmission de couple pour véhicule automobile.In the current technique, the annular mass of a flexible flywheel is generally formed by a cast iron ring fixed by screws or rivets on the radially external periphery of a flexible annular sheet, the radially internal peripheral part of which comprises fixing screw passage holes on the driving shaft, that is to say on the crankshaft of an internal combustion engine in the case of a torque transmission device for a motor vehicle.
La tôle annulaire flexible a une épaisseur relativement faible (de l'ordre de 2 à 3 mm par exemple) et sa partie périphérique radialement interne de fixation sur l'arbre menant est renforcée par une rondelle de rigidification ayant une épaisseur plus importante et sur laquelle les têtes des vis de fixation peuvent s'appuyer. Cette tôle annulaire de faible épaisseur doit être contrôlée après découpe, éventuellement redressée et assemblée avec soin à la masse annulaire en fonte. Ces opérations sont relativement longues et délicates et sont donc coûteuses. On a constaté qu'en fonctionnement, un volant de ce type se déforme en flexion de "pompage" (déformation en flexion dans laquelle le volant flexible reste sensiblement parallèle à lui-même) et en oscillation autour d'un axe qui est perpendiculaire à l'axe de rotation du volant et qui a une position angulaire déterminée par rapport au vilebrequin, cette oscillation étant liée à une flexion du dernier maneton du vilebrequin. Les volants flexibles connus sont caractérisés par une structure à symétrie de révolution et ne sont donc pas conçus pour prendre en compte ce phénomène d'oscillation.The flexible annular sheet has a relatively small thickness (of the order of 2 to 3 mm for example) and its radially internal peripheral part for fixing to the driving shaft is reinforced by a stiffening washer having a greater thickness and on which heads fixing screws can be supported. This thin annular sheet must be checked after cutting, possibly straightened and carefully assembled with the annular mass in cast iron. These operations are relatively long and delicate and are therefore expensive. It has been found that in operation, a flywheel of this type deforms in "pumping" bending (bending deformation in which the flexible flywheel remains substantially parallel to itself) and in oscillation around an axis which is perpendicular to the axis of rotation of the flywheel and which has a determined angular position relative to the crankshaft, this oscillation being linked to a bending of the last crankpin of the crankshaft. Known flexible flywheels are characterized by a structure with symmetry of revolution and are therefore not designed to take this oscillation phenomenon into account.
L'invention a notamment pour objet un volant flexible qui répond à ce besoin et qui ne présente pas les inconvénients des volants flexibles de la technique antérieure.The invention particularly relates to a flexible steering wheel which meets this need and which does not have the drawbacks of the flexible steering wheels of the prior art.
Elle propose à cet effet un volant d'inertie flexible pour dispositif de transmission de couple, en particulier pour véhicule automobile, destiné à être entraîné autour d'un axe de rotation par un arbre menant et comprenant une masse annulaire portée par un élément flexible destiné à être fixé à l'arbre menant, caractérisé en ce que cet élément flexible comprend des bras radiaux définissant un axe privilégié d'oscillation perpendiculaire à l'axe de rotation du volant.To this end, it provides a flexible flywheel for a torque transmission device, in particular for a motor vehicle, intended to be driven around an axis of rotation by a drive shaft and comprising an annular mass carried by a flexible element intended to be fixed to the driving shaft, characterized in that this flexible element comprises radial arms defining a preferred axis of oscillation perpendicular to the axis of rotation of the flywheel.
Le volant flexible selon l'invention est donc particulièrement conçu pour répondre au phénomène d'oscillation précité et pour l'absorber, au moins en partie, en découplant de l'arbre menant le volant oscillant autour de l'axe privilégié.The flexible flywheel according to the invention is therefore particularly designed to respond to the aforementioned oscillation phenomenon and to absorb it, at least in part, by decoupling from the shaft driving the flywheel oscillating around the preferred axis.
En pratique, les bras radiaux de l'élément flexible peuvent être avantageusement formés par une surépaisseur locale de cet élément flexible. En d'autres termes, l'élément flexible a une épaisseur supérieure dans ses parties qui forment les bras radiaux, et il a une épaisseur plus faible dans ses autres parties, cette épaisseur plus faible pouvant être réduite et même annulée dès lors que les bras radiaux ont une épaisseur et une rigidité suffisante pour assurer la transmission du couple entre l'arbre menant et l'arbre mené. L'élément flexible du volant flexible selon l'invention peut alors être formé d'une tôle plus épaisse que dans la technique antérieure, qui peut être d'une qualité inférieure et qui n'a pas besoin de pré-traitement, qui est plus facile à travailler, qui se déforme moins et que l'on n'a pas besoin de redresser, de sorte que le volant selon l'invention est moins coûteux que dans la technique antérieure.In practice, the radial arms of the flexible element can advantageously be formed by a local excess thickness of this flexible element. In other words, the flexible element has a greater thickness in its parts which form the radial arms, and it has a greater thickness. low in its other parts, this smaller thickness can be reduced and even canceled as soon as the radial arms have a thickness and a rigidity sufficient to ensure the transmission of the torque between the driving shaft and the driven shaft. The flexible element of the flexible steering wheel according to the invention can then be formed from a thicker sheet than in the prior art, which can be of a lower quality and which does not need pretreatment, which is more easy to work, which deforms less and which does not need to be straightened, so that the steering wheel according to the invention is less expensive than in the prior art.
Cela permet aussi de fabriquer l'élément flexible d'une seule pièce avec la masse annulaire, notamment en fonte d'une qualité résistant aux contraintes en flexion et en torsion, ce qui évite tous les problèmes et les inconvénients liés à la fabrication séparée de la masse annulaire et de l'élément flexible et à leur assemblage.This also makes it possible to manufacture the flexible element in a single piece with the annular mass, in particular of cast iron of a quality resistant to the flexural and torsional stresses, which avoids all the problems and drawbacks associated with the separate manufacture of the annular mass and the flexible element and their assembly.
Selon d'autres caractéristiques de l'invention, l'axe d'oscillation est formé de deux bras radiaux qui s'étendent dans le prolongement l'un de l'autre sensiblement entre l'axe de rotation et la masse annulaire d'inertie ou bien de trois bras radiaux dont deux sont symétriques l'un de l'autre par rapport au prolongement du troisième, ces trois bras radiaux s'étendant chacun entre l'axe de rotation et la masse annulaire.According to other characteristics of the invention, the axis of oscillation is formed by two radial arms which extend in line with one another substantially between the axis of rotation and the annular mass of inertia or else three radial arms, two of which are symmetrical to each other with respect to the extension of the third, these three radial arms each extending between the axis of rotation and the annular mass.
Dans une première forme de réalisation, l'élément flexible est formé d'un disque comportant des évidements symétriques formés de part et d'autre de l'axe d'oscillation. Ces évidements peuvent être traversants ou non.In a first embodiment, the flexible element is formed of a disc having symmetrical recesses formed on either side of the axis of oscillation. These recesses can be through or not.
Lorsque l'élément flexible n'est pas formé d'une seule pièce avec la masse annulaire, il est fixé à celle-ci par des vis, rivets ou analogues, aux extrémités des bras radiaux précités.When the flexible element is not formed in one piece with the annular mass, it is fixed to the latter by screws, rivets or the like, at the ends of the above-mentioned radial arms.
L'élément flexible peut être formé soit d'un seul élément en tôle d'une épaisseur voulue, soit de plusieurs éléments plats superposés et fixés ensemble sur la masse annulaire. Selon une autre caractéristique de l'invention, le volant flexible comprenant des moyens d'hystérésis portés par l'élément flexible et coopérant par frottement avec la masse annulaire.The flexible element can be formed either of a single sheet metal element of a desired thickness, or of several flat elements superimposed and fixed together on the annular mass. According to another characteristic of the invention, the flexible flywheel comprising hysteresis means carried by the flexible element and cooperating by friction with the annular mass.
Dans un mode de réalisation, ces moyens d'hystérésis comprennent deux bras radiaux s'étendant perpendiculairement à l'axe d'oscillation et ayant des extrémités radialement internes solidaires de l'élément flexible et des extrémités radialement externes en contact avec la masse annulaire.In one embodiment, these hysteresis means comprise two radial arms extending perpendicular to the axis of oscillation and having radially internal ends integral with the flexible element and radially external ends in contact with the annular mass.
Les bras radiaux des moyens d'hystérésis sont formés d'une seule pièce avec l'élément flexible ou, en variante, font partie d'une rondelle rapportée sur l'élément flexible, cette rondelle étant destinée à être fixée avec l'élément flexible sur l'arbre menant.The radial arms of the hysteresis means are formed in one piece with the flexible element or, as a variant, are part of a washer attached to the flexible element, this washer being intended to be fixed with the flexible element. on the leading tree.
Dans un autre mode de réalisation, les moyens d'hystérésis comprennent des goupilles élastiques montées dans des logements semi- cylindriques de deux pattes solidaires de l'élément flexible et de deux pattes solidaires de la masse annulaire, ces pattes s'étendant dans une direction perpendiculaire à l'axe d'oscillation précité.In another embodiment, the hysteresis means comprise elastic pins mounted in semi-cylindrical housings with two lugs secured to the flexible element and two lugs secured to the annular mass, these lugs extending in one direction perpendicular to the above-mentioned axis of oscillation.
Selon encore une autre caractéristique de l'invention, les bras radiaux qui définissent l'axe d'oscillation comportent entre leurs extrémités radialement internes et radialement externes, des découpes ou encoches de localisation de contraintes maximales.According to yet another characteristic of the invention, the radial arms which define the axis of oscillation comprise, between their radially internal and radially external ends, cutouts or notches for locating maximum stresses.
Cela permet d'éloigner les contraintes maximales des zones de fixation ou de raccordement des bras radiaux à la masse annulaire.This removes the maximum stresses from the areas of attachment or connection of the radial arms to the annular mass.
Les bras radiaux précités peuvent s'étendre perpendiculairement à l'axe de rotation ou peuvent être légèrement inclinés en oblique par rapport à une perpendiculaire à l'axe de rotation, par exemple dans une direction opposée à l'arbre menant à partir de leurs extrémités radialement internes.The aforementioned radial arms may extend perpendicular to the axis of rotation or may be slightly inclined obliquely relative to a perpendicular to the axis of rotation, for example in a direction opposite to the shaft leading from their ends radially internal.
Selon encore une autre caractéristique de l'invention, l'élément flexible comprend des moyens définissant un second axe d'oscillation qui est perpendiculaire à l'axe de rotation et au premier axe d'oscillation cité. Les deux axes d'oscillation sont définis par des bras radiaux de l'élément flexible. Dans un mode de réalisation particulier de l'invention, ces bras radiaux sont reliés à la masse annulaire par des languettes qui ont des raideurs différentes selon qu'elles relient à la masse annulaire les bras radiaux définissant le premier axe d'oscillation ou ceux définissant le second axe d'oscillation.According to yet another characteristic of the invention, the flexible element comprises means defining a second axis of oscillation which is perpendicular to the axis of rotation and to the first axis of oscillation mentioned. The two axes of oscillation are defined by radial arms of the flexible element. In a particular embodiment of the invention, these radial arms are connected to the annular mass by tongues which have different stiffnesses depending on whether they connect to the annular mass the radial arms defining the first axis of oscillation or those defining the second axis of oscillation.
Le volant flexible selon l'invention peut notamment former le volant primaire d'un double volant amortisseur qui comprend également un volant d'inertie secondaire destiné à être relié à l'arbre d'entrée d'une transmission par un embrayage et un amortisseur de torsion monté entre les deux volants d'inertie.The flexible flywheel according to the invention can in particular form the primary flywheel of a double damper flywheel which also comprises a secondary flywheel intended to be connected to the input shaft of a transmission by a clutch and a shock absorber of torsion mounted between the two flywheels.
Dans un mode de réalisation de l'invention, l'amortisseur de torsion est du type comprenant des ressorts orientés radialement par rapport à l'axe de rotation, dans la position de repos du double volant amortisseur.In one embodiment of the invention, the torsion damper is of the type comprising springs oriented radially with respect to the axis of rotation, in the rest position of the double damping flywheel.
Les moyens d'hystérésis associés au volant primaire flexible comprennent avantageusement une rondelle élastique qui est portée par l'élément flexible du volant primaire et qui vient en appui sur ce dernier, ou bien qui est montée entre l'élément flexible du volant primaire et la masse annulaire portée par cet élément flexible.The hysteresis means associated with the flexible primary flywheel advantageously comprise an elastic washer which is carried by the flexible element of the primary flywheel and which comes to bear on the latter, or else which is mounted between the flexible element of the primary flywheel and the annular mass carried by this flexible element.
L'invention sera mieux comprise et d'autres caractéristiques, détails et avantages de celle-ci apparaîtront plus clairement à la lecture de la description qui suit, faite à titre d'exemple en référence aux dessins annexés dans lesquels : la figure 1 est une schématique de face d'un volant flexible selon l'invention ; - la figure 2 est une vue schématique en coupe axiale du volant de la figure 1 ; les figures 3 et 4 sont des vues semblables aux figures 1 et 2, pour une variante de réalisation du volant flexible ; les figures 5 et 6 sont des vues semblables aux figures 1 et 2 pour une autre variante de réalisation ; la figure 7 est une vue schématique en coupe axiale d'une autre variante de réalisation du volant flexible ; la figure 8 est une vue schématique en perspective du volant de la figure 7 ; - les figures 9 et 10 sont des vues semblables aux figures 1 et 2 pour une autre variante de réalisation de l'invention ;The invention will be better understood and other characteristics, details and advantages thereof will appear more clearly on reading the description which follows, given by way of example with reference to the appended drawings in which: FIG. 1 is a schematic front view of a flexible steering wheel according to the invention; - Figure 2 is a schematic view in axial section of the steering wheel of Figure 1; Figures 3 and 4 are views similar to Figures 1 and 2, for an alternative embodiment of the flexible steering wheel; Figures 5 and 6 are views similar to Figures 1 and 2 for another alternative embodiment; Figure 7 is a schematic view in axial section of another alternative embodiment of the flexible flywheel; Figure 8 is a schematic perspective view of the steering wheel of Figure 7; - Figures 9 and 10 are views similar to Figures 1 and 2 for another alternative embodiment of the invention;
La figure 11 représente schématiquement une disposition d'éléments flexibles consécutifs dans une bande de tôle avant découpe ;FIG. 11 schematically represents an arrangement of consecutive flexible elements in a sheet metal strip before cutting;
La figure 12 est une vue schématique en élévation d'une autre variante de réalisation du volant flexible ;Figure 12 is a schematic elevational view of another alternative embodiment of the flexible flywheel;
La figure 13 est une vue schématique en perspective du volant de la figure 12 ;Figure 13 is a schematic perspective view of the steering wheel of Figure 12;
La figure 14 est une vue schématique de face d'une autre variante de réalisation du volant flexible ; - Les figures 15 et 16 sont des vues schématiques en coupe selon les lignes XV-XV et XVI-XVI respectivement de la figure 14 ;Figure 14 is a schematic front view of another alternative embodiment of the flexible steering wheel; - Figures 15 and 16 are schematic sectional views along lines XV-XV and XVI-XVI respectively of Figure 14;
La figure 17 est une vue schématique de face d'encore une autre variante de réalisation du volant flexible ;Figure 17 is a schematic front view of yet another alternative embodiment of the flexible steering wheel;
Les figures 18 et 19 sont des vues schématiques en coupe axiale dans deux plans perpendiculaires du volant de la figure 17 ;Figures 18 and 19 are schematic views in axial section in two perpendicular planes of the steering wheel of Figure 17;
La figure 20 est une schématique de face d'encore une autre variante de réalisation du volant flexible ;Figure 20 is a schematic front view of yet another alternative embodiment of the flexible steering wheel;
La figure 21 est une vue schématique partielle en coupe axiale, à plus grande échelle, du volant de la figure 20 ; - La figure 22 est une vue schématique de face d'une autre variante de réalisation du volant flexible sur l'invention ;Figure 21 is a partial schematic view in axial section, on a larger scale, of the steering wheel of Figure 20; - Figure 22 is a schematic front view of another alternative embodiment of the flexible steering wheel on the invention;
La figure 23 est une vue schématique en coupe axiale d'un double volant amortisseur selon l'invention ;Figure 23 is a schematic view in axial section of a double damping flywheel according to the invention;
La figure 24 est une demi-vue schématique en coupe axiale d'une variante de réalisation du double volant amortisseur ; Les figures 25 et 26 sont des vues schématiques en coupe axiale de deux autres variantes de réalisation du double volant amortisseur selon l'invention ;Figure 24 is a schematic half-view in axial section of an alternative embodiment of the double damping flywheel; Figures 25 and 26 are schematic views in axial section of two other alternative embodiments of the double damping flywheel according to the invention;
La figure 27 est une vue schématique du volant de la figure 1 décrivant son positionnement par rapport à l'arbre menant.Figure 27 is a schematic view of the steering wheel of Figure 1 describing its positioning relative to the drive shaft.
On se réfère d'abord aux figures 1 et 2 dans lesquelles on a représenté schématiquement un premier mode de réalisation d'un volant flexible selon l'invention. Ce volant flexible, désigné généralement par la référence 10, est destiné à la transmission d'un couple entre un arbre menant 12 qui est le vilebrequin d'un moteur à combustion interne de véhicule automobile, et un arbre mené (non représenté) qui est l'arbre d'entrée d'une boîte de vitesses par exemple, et qui est destiné à être monté solidaire en rotation d'un moyeu 14 d'un amortisseur de torsion coaxial au volant d'inertie 10 et à l'arbre menant 12.Reference is first made to FIGS. 1 and 2 in which a first embodiment of a flexible flywheel according to the invention is shown diagrammatically. This flexible flywheel, generally designated by the reference 10, is intended for the transmission of a torque between a driving shaft 12 which is the crankshaft of an internal combustion engine of a motor vehicle, and a driven shaft (not shown) which is the input shaft of a gearbox for example, and which is intended to be mounted integral in rotation with a hub 14 of a torsional damper coaxial with the flywheel 10 and the driving shaft 12 .
Le moyeu 14 de l'amortisseur de torsion est, de façon connue, relié par un embrayage E au volant d'inertie 10 dont une face radiale 16 orientée du côté opposé à l'arbre menant 12 forme une surface de friction coopérant avec le disque de friction 18 de l'embrayage E.The hub 14 of the torsion damper is, in known manner, connected by a clutch E to the flywheel 10, a radial face 16 oriented on the side opposite to the drive shaft 12 forms a friction surface cooperating with the disc clutch 18 of clutch E.
Le volant d'inertie 10 selon l'invention est fixé en bout de l'arbre menant 12 par des vis 20, orientées parallèlement à l'axe 22 de rotation de l'arbre 12 et du volant 10, et réparties de façon régulière en cercle autour de cet axe 22. Les vis 20 sont reçues dans des orifices 24 d'une partie annulaire radialement interne 26 du volant d'inertie 10, cette partie annulaire 26 étant reliée par deux bras radiaux 28 diamétralement opposés à une masse annulaire 30 qui entoure la partie annulaire 26 et dont la périphérie cylindrique externe porte des cibles d'allumage 32. Dans ce mode de réalisation, la partie annulaire 26, les bras radiauxThe flywheel 10 according to the invention is fixed at the end of the driving shaft 12 by screws 20, oriented parallel to the axis 22 of rotation of the shaft 12 and of the flywheel 10, and distributed evenly in circle around this axis 22. The screws 20 are received in orifices 24 of a radially internal annular part 26 of the flywheel 10, this annular part 26 being connected by two radial arms 28 diametrically opposite to an annular mass 30 which surrounds the annular part 26 and whose external cylindrical periphery carries ignition targets 32. In this embodiment, the annular part 26, the radial arms
28 et la masse annulaire 30 sont formés d'une seule pièce en fonte d'acier d'une qualité résistant aux contraintes de flexion par exemple en fonte à graphite sphéroïdal.28 and the annular mass 30 are formed in a single piece of cast steel of a quality resistant to bending stresses, for example in spheroidal graphite cast iron.
Les bras 28 ne sont pas exactement perpendiculaires à l'axe de rotation 22, mais sont inclinés légèrement en oblique et s'étendent vers l'embrayage à partir de la partie annulaire 26. Cela permet d'augmenter la raideur axiale du volant qui résiste mieux aux efforts de débrayage, et d'augmenter la fréquence de pompage.The arms 28 are not exactly perpendicular to the axis of rotation 22, but are inclined slightly obliquely and extend towards the clutch from the annular part 26. This makes it possible to increase the axial stiffness of the flywheel which resists better with declutching efforts, and increase the pumping frequency.
Les bras radiaux 28 ont des dimensions en largeur et en épaisseur qui permettent de transmettre le couple maximal généré par le moteur à combustion interne du véhicule automobile.The radial arms 28 have dimensions in width and in thickness which make it possible to transmit the maximum torque generated by the internal combustion engine of the motor vehicle.
Ils définissent par ailleurs un axe d'oscillation 34 qui est perpendiculaire à l'axe de rotation 22 et dont la position angulaire autour de cet axe est déterminée par rapport à l'arbre menant 12 et est connue par mesure ou par calcul (la position angulaire du volant d'inertie 10 par rapport à l'arbre menant 12 étant elle-même fixée et déterminée au montage par des moyens appropriés).They also define an axis of oscillation 34 which is perpendicular to the axis of rotation 22 and whose angular position around this axis is determined relative to the drive shaft 12 and is known by measurement or by calculation (the position angular of the flywheel 10 relative to the driving shaft 12 being itself fixed and determined for mounting by appropriate means).
La partie annulaire 26 et les bras radiaux 28 du volant d'inertie définissent un élément flexible, semblable à la tôle annulaire flexible d'un volant d'inertie flexible de la technique antérieure, permettant des déformations du volant d'inertie en flexion (la masse annulaire 30 se déplaçant alors parallèlement à elle-même).The annular part 26 and the radial arms 28 of the flywheel define a flexible element, similar to the flexible annular sheet of a flexible flywheel of the prior art, allowing deformations of the flywheel in bending (the annular mass 30 then moving parallel to itself).
Les bras radiaux 28 du volant d'inertie 10 permettent également une oscillation de ce volant autour de l'axe 34, cette oscillation étant liée à une flexion du dernier maneton du vilebrequin formant l'arbre menant 12. La section des bras radiaux 28 est déterminée par exemple pour autoriser ce phénomène d'oscillation à une fréquence de vibration du vilebrequin qui correspond à une vitesse de rotation de 2700 à 4500 tours par minute environ.The radial arms 28 of the flywheel 10 also allow an oscillation of this flywheel about the axis 34, this oscillation being linked to a bending of the last crankpin of the crankshaft forming the driving shaft 12. The section of the radial arms 28 is determined for example to allow this oscillation phenomenon at a vibration frequency of the crankshaft which corresponds to a rotation speed of approximately 2700 to 4500 revolutions per minute.
Dans un mode de réalisation de l'invention, le diamètre de la friction est de 220 mm, les bras radiaux 28 ont une section transversale de forme oblongue ou sensiblement rectangulaire à extrémités arrondies, le volant d'inertie est réalisé en fonte à graphite sphéroïdal ayant une résistance à la rupture de l'ordre de 500 MPa et les bras radiaux 28 ont une épaisseur de 6 à 10 mm pour une largeur de 30 à 40 mm. Les rayons des raccordements 36 des bras radiaux à la masse annulaire 30 sont déterminés pour réduire les concentrations de contraintes et sont par exemple de 8 mm environ.In one embodiment of the invention, the diameter of the friction is 220 mm, the radial arms 28 have a cross section of oblong or substantially rectangular shape with rounded ends, the flywheel of inertia is made of spheroidal graphite cast iron having a breaking strength of the order of 500 MPa and the radial arms 28 have a thickness of 6 to 10 mm for a width of 30 to 40 mm. The radii of the connections 36 of the radial arms to the annular mass 30 are determined to reduce the stress concentrations and are for example approximately 8 mm.
L'amortissement dans la fonte à graphite sphéroïdal est approximativement trois ou quatre fois supérieur à l'amortissement dans l'acier.The damping in spheroidal graphite cast iron is approximately three or four times greater than the damping in steel.
Dans la variante de réalisation représentée aux figures 3 et 4, l'axe d'oscillation 34 du volant d'inertie 10 est défini par un bras radial 28 identique à ceux déjà décrits et par deux autres bras radiaux 40 qui sont symétriques l'un de l'autre par rapport à l'axe 34 et qui s'étendent dans des directions sensiblement opposées à celle du bras radial 28 par rapport à l'axe de rotation 22, ces bras radiaux 40 faisant un angle d'environ 140 degrés avec le bras radial 28 dans l'exemple représenté.In the embodiment shown in Figures 3 and 4, the axis of oscillation 34 of the flywheel 10 is defined by a radial arm 28 identical to those already described and by two other radial arms 40 which are symmetrical one on the other relative to the axis 34 and which extend in directions substantially opposite to that of the radial arm 28 relative to the axis of rotation 22, these radial arms 40 making an angle of about 140 degrees with the radial arm 28 in the example shown.
Ces deux bras radiaux 40 sont un peu plus faciles à réaliser de fonderie qu'un unique bras radial 28 et peuvent réduire également les problèmes de retrait de moulage.These two radial arms 40 are a little easier to foundry than a single radial arm 28 and can also reduce the problems of molding shrinkage.
Pour le reste, la structure du volant d'inertie 10 représentée aux figures 3 et 4 est identique à celle du volant d'inertie des figures 1 et 2.For the rest, the structure of the flywheel 10 shown in FIGS. 3 and 4 is identical to that of the flywheel in FIGS. 1 and 2.
Dans le mode de réalisation des figures 5 et 6, le volant d'inertie 10 est du type représenté aux figures 1 et 2 et est associé à des moyens d'hystérésis permettant d'amortir les oscillations du volant autour de l'axe 34 défini par les bras radiaux 28. Ces moyens d'hystérésis comprennent une rondelle élastique 42 de forme annulaire, réalisée par exemple en acier à ressort et destinée à être fixée sur l'extrémité de l'arbre menant précité en même temps que la partie annulaire radialement interne 26 du volant d'inertie. A cet effet, la rondelle élastique 42 comporte des orifices 44 coïncidant avec les orifices 24 formés dans la partie annulaire 26 pour le passage des vis de fixation 20, et son diamètre interne est sensiblement égal à celui de la partie annulaire 26 du volant d'inertie.In the embodiment of FIGS. 5 and 6, the flywheel 10 is of the type shown in FIGS. 1 and 2 and is associated with hysteresis means making it possible to dampen the oscillations of the flywheel around the defined axis 34 by the radial arms 28. These hysteresis means comprise an elastic washer 42 of annular shape, made for example of spring steel and intended to be fixed on the end of the aforementioned driving shaft at the same time as the annular part radially internal 26 of the flywheel. For this purpose, the elastic washer 42 has orifices 44 coinciding with the orifices 24 formed in the annular part 26 for the passage of the fixing screws 20, and its internal diameter is substantially equal to that of the annular part 26 of the flywheel.
Cette rondelle élastique 42 comporte deux bras radiaux 46 diamétralement opposés, qui s'étendent dans une direction perpendiculaire à l'axe d'oscillation 34 et dont les extrémités radialement externes 48 sont recourbées parallèlement à l'axe pour venir s'appliquer à pression sur la surface cylindrique interne 50 de la masse annulaire 30.This elastic washer 42 comprises two diametrically opposite radial arms 46, which extend in a direction perpendicular to the axis of oscillation 34 and whose radially external ends 48 are bent parallel to the axis to come to apply pressure on the internal cylindrical surface 50 of the annular mass 30.
Dans ces conditions, en fonctionnement, toute oscillation de la masse annulaire 30 autour de l'axe 34 se traduit par un frottement sur les extrémités repliées 48 des bras de la rondelle élastique 42 solidaire de la partie annulaire radialement interne 26 du volant d'inertie.Under these conditions, in operation, any oscillation of the annular mass 30 around the axis 34 results in friction on the folded ends 48 of the arms of the elastic washer 42 secured to the radially internal annular part 26 of the flywheel .
Dans une variante de réalisation, les extrémités 48 des bras 46 s'étendent au travers de petits orifices formés dans un voile reliant la partie annulaire 26 à la masse annulaire 30. Dans le mode de réalisation des figures 7 et 8, le volant d'inertie 10 selon l'invention est formé de deux éléments indépendants qui sont fixés l'un à l'autre, à savoir un élément flexible 52 réalisé en tôle d'acier et une masse annulaire d'inertie 30 réalisée en fonte, l'élément flexible 52 étant de forme générale annulaire et étant fixé à sa périphérie radialement externe sur la masse d'inertie 30 par des vis 54, des rivets ou analogues.In an alternative embodiment, the ends 48 of the arms 46 extend through small orifices formed in a veil connecting the annular part 26 to the annular mass 30. In the embodiment of FIGS. 7 and 8, the flywheel inertia 10 according to the invention is formed of two independent elements which are fixed to each other, namely a flexible element 52 made of sheet steel and an annular mass of inertia 30 made of cast iron, the element flexible 52 being of generally annular shape and being fixed at its radially outer periphery to the mass of inertia 30 by screws 54, rivets or the like.
L'élément flexible 52 comprend une partie annulaire radialement interne 56, formée avec des orifices 58 de passage des vis de fixation sur l'extrémité de l'arbre menant, une partie annulaire radialement externe 60 comportant des orifices de passage des vis 54 de fixation sur la masse annulaire 30, et deux bras radiaux 62 diamétralement opposés, qui relient entre elles les parties annulaires 56 et 60.The flexible element 52 comprises a radially internal annular part 56, formed with holes 58 for the passage of the fixing screws on the end of the driving shaft, a radially external annular part 60 comprising holes for the passage of the fixing screws 54 on the annular mass 30, and two radially opposite radial arms 62, which connect the annular parts 56 and 60 together.
Préférentiellement, l'élément flexible 52 est formé d'une rondelle annulaire dans laquelle sont pratiquées deux découpes 64 diamétralement opposées, sensiblement en forme de haricot, qui définissent entre elles les bras radiaux 62. Typiquement, l'élément flexible 52 est formé d'une tôle d'acier qui a une épaisseur nettement supérieure à celle des tôles d'acier formant les éléments flexibles des volants d'inertie flexibles de la technique antérieure, cette épaisseur étant par exemple de l'ordre de 5 mm. Cette épaisseur réduit les risques de déformation de la tôle lors de son usinage et facilite et simplifie la fabrication de l'élément flexible 52.Preferably, the flexible element 52 is formed of an annular washer in which two diametrically opposed cutouts 64 are formed, substantially in the shape of a bean, which define between them the radial arms 62. Typically, the flexible element 52 is formed from a steel sheet which has a thickness considerably greater than that of the steel sheets forming the flexible elements of the flexible flywheels of the prior art, this thickness being for example of around 5 mm. This thickness reduces the risks of deformation of the sheet during its machining and facilitates and simplifies the manufacture of the flexible element 52.
Comme précédemment, l'axe d'oscillation du volant est défini par l'axe diamétral de symétrie des bras radiaux 62.As before, the axis of oscillation of the flywheel is defined by the diametrical axis of symmetry of the radial arms 62.
Dans la variante de réalisation des figures 9 et 10, l'élément flexible 72 du volant d'inertie 10 selon l'invention est formé essentiellement d'une partie annulaire interne 74 qui comporte les orifices 76 de passage des vis de fixation sur l'extrémité de l'arbre menant, de deux bras radiaux 78 du type précité qui définissent l'axe d'oscillation du volant d'inertie et qui ont des prolongements 80 radiaux vers l'extérieur, ces prolongements 80 formant des zones de fixation sur la masse annulaire 30 et comportant à cet effet des orifices de passage de vis de fixation 82, de rivets ou analogues.In the alternative embodiment of FIGS. 9 and 10, the flexible element 72 of the flywheel 10 according to the invention is essentially formed by an internal annular part 74 which includes the orifices 76 for the passage of the fixing screws on the end of the driving shaft, of two radial arms 78 of the aforementioned type which define the axis of oscillation of the flywheel and which have radial extensions 80 towards the outside, these extensions 80 forming fixing zones on the annular mass 30 and comprising for this purpose holes for fixing screw 82, rivets or the like.
Des échancrures ou des découpes 84 sont formées dans les côtés des bras radiaux 78, pour constituer des zones de localisation de contraintes maximales et écarter ces contraintes maximales des orifices de passage des vis 82.Notches or cutouts 84 are formed in the sides of the radial arms 78, in order to constitute zones for locating maximum stresses and to separate these maximum stresses from the orifices for the passage of screws 82.
La figure 11 représente schématiquement une succession d'éléments flexibles tels que l'élément 52 des figures 7 et 8, et dont le bord périphérique extérieur 86 comporte une echancrure 88 et une pointe 90 diamétralement opposées, cette pointe et cette echancrure permettant d'imbriquer partiellement les uns dans les autres les éléments flexibles 52 lors de leur formation dans une bande de tôle.FIG. 11 schematically represents a succession of flexible elements such as the element 52 of FIGS. 7 and 8, and the outer peripheral edge 86 of which has a notch 88 and a point 90 diametrically opposite, this point and this notch making it possible to nest partially in each other the flexible elements 52 during their formation in a sheet metal strip.
Comme représenté en figure 11, la pointe 90 d'un élément 52 s'étend à l'intérieur de l'échancrure 88 de l'élément 52 suivant et ainsi de suite. Pour gagner de la place et donc de la matière, la pointe 90 de chaque élément flexible 52 est elle-même formée par deux échancrures incurvées 92 pratiquées dans la partie annulaire radialement externe 60 de l'élément flexible. Dans le mode de réalisation des figures 12 et 13, l'élément flexible du volant d'inertie 10 selon l'invention est du même type que l'élément flexible 72 des figures 9 et 10 et est associé à des moyens d'hystérésis formés par un élément élastique 96 en forme de croix, qui s'étend dans un plan perpendiculaire à l'axe de rotation et qui est appliqué sur l'élément 72. Cet élément élastique 96 comporte deux bras radiaux 98 diamétralement opposés, qui ont la même forme que les bras radiaux 78 de l'élément flexible 72 et qui sont superposés à ces derniers et deux autres bras radiaux 100 perpendiculaires aux bras radiaux 98 et ayant une extrémité radialement externe 102 appuyée sur une face radiale de la masse d'inertie 30 pour générer un amortissement par frottement radial lors des oscillations du volant d'inertie autour de l'axe défini par les bras radiaux 78 et 98.As shown in FIG. 11, the tip 90 of an element 52 extends inside the notch 88 of the next element 52 and so on. To save space and therefore material, the tip 90 of each flexible element 52 is itself formed by two curved notches 92 formed in the radially external annular part 60 of the flexible element. In the embodiment of Figures 12 and 13, the flexible element of the flywheel 10 according to the invention is of the same type as the flexible element 72 of Figures 9 and 10 and is associated with hysteresis means formed by an elastic element 96 in the shape of a cross, which extends in a plane perpendicular to the axis of rotation and which is applied to the element 72. This elastic element 96 comprises two radially opposite radial arms 98, which have the same forms that the radial arms 78 of the flexible element 72 and which are superimposed on the latter and two other radial arms 100 perpendicular to the radial arms 98 and having a radially external end 102 supported on a radial face of the inertia mass 30 for generate a damping by radial friction during the oscillations of the flywheel around the axis defined by the radial arms 78 and 98.
L'élément élastique 96 est fixé aux extrémités de ses bras radiaux 98 sur la masse annulaire 30 par les vis 82 de fixation de l'élément flexible 72, et sa partie annulaire radialement interne comporte des orifices 104 de passage des vis de fixation du volant d'inertie sur l'arbre menant.The elastic element 96 is fixed at the ends of its radial arms 98 to the annular mass 30 by the screws 82 for fixing the flexible element 72, and its radially internal annular part includes orifices 104 for passage of the steering wheel fixing screws. of inertia on the leading tree.
Dans ce mode de réalisation, l'élément flexible 72 peut être formé par un empilement d'éléments plats allongés en tôle mince, et l'élément élastique 96 fait partie de l'empilement.In this embodiment, the flexible element 72 can be formed by a stack of elongated flat elements made of thin sheet, and the elastic element 96 is part of the stack.
Dans le mode de réalisation des figures 14, 15 et 16, le volant d'inertie 10 est réalisé d'une seule pièce, par exemple en fonte, et sa partie annulaire radialement interne 26 est reliée à la masse annulaire 30 par deux bras radiaux 28 diamétralement opposés semblables à ceux du mode de réalisation des figures 1 et 2, et par un voile annulaire 108 d'épaisseur relativement faible, qui occupe tout l'espace entre la partie annulaire 26, la masse annulaire 30 et les bras radiaux 28. L'élément flexible du volant est alors un anneau comportant des surépaisseurs locales formant les bras radiaux 28.In the embodiment of FIGS. 14, 15 and 16, the flywheel 10 is made in one piece, for example of cast iron, and its radially internal annular part 26 is connected to the annular mass 30 by two radial arms 28 diametrically opposite, similar to those of the embodiment of FIGS. 1 and 2, and by an annular web 108 of relatively small thickness, which occupies the entire space between the annular part 26, the annular mass 30 and the radial arms 28. The flexible element of the steering wheel is then a ring comprising local excess thicknesses forming the radial arms 28.
Pour le reste, ce volant d'inertie a la même structure que celui des figures 1 et 2. Dans le mode de réalisation des figures 17 et 19, le volant flexible 10 comprend une masse annulaire 30 en fonte et un élément flexible du type représenté aux figures 9 et 10, cet élément flexible étant formé d'un empilage d'éléments identiques 72 réalisés en tôle mince.For the rest, this flywheel has the same structure as that of FIGS. 1 and 2. In the embodiment of FIGS. 17 and 19, the flexible flywheel 10 comprises an annular mass 30 in cast iron and a flexible element of the type shown. Figures 9 and 10, this flexible element being formed of a stack of identical elements 72 made of thin sheet.
Comme dans le mode de réalisation des figures 9 et 10, cet élément flexible est fixé à la masse annulaire 30 par des vis 82, des rivets ou analogues aux extrémités 80 de ses bras radiaux 78 définissant l'axe d'oscillation.As in the embodiment of Figures 9 and 10, this flexible element is fixed to the annular mass 30 by screws 82, rivets or the like at the ends 80 of its radial arms 78 defining the axis of oscillation.
Comme on le voit mieux en figure 19, l'empilement d'éléments identiques 72 est appliqué sur une tôle annulaire mince 110 fixée à la masse annulaire 30 par les vis 82 de fixation des éléments flexibles 72, la périphérie de cette tôle annulaire mince 110 étant en appui sur une face radiale de la masse annulaire 30 et constituant ainsi des moyens d'hystérésis pour l'amortissement des flexions et des oscillations du volant d'inertie. Les éléments empilés 72 peuvent avoir des épaisseurs différentes, plus importantes au milieu de l'empilement qu'à ses extrémités, pour égaliser les contraintes en flexion. Les duretés des éléments empilés peuvent aussi être différentes.As best seen in FIG. 19, the stack of identical elements 72 is applied to a thin annular sheet 110 fixed to the annular mass 30 by the screws 82 for fixing the flexible elements 72, the periphery of this thin annular sheet 110 being supported on a radial face of the annular mass 30 and thus constituting hysteresis means for damping the flexions and oscillations of the flywheel. The stacked elements 72 can have different thicknesses, greater in the middle of the stack than at its ends, to equalize the bending stresses. The hardnesses of the stacked elements can also be different.
Dans le mode de réalisation des figures 20 et 21, le volant d'inertie flexible 10 est réalisé en une seule pièce et comprend une partie annulaire radialement interne 26 reliée par deux bras radiaux 28 diamétralement opposés à une masse annulaire 30, comme dans les modes de réalisation déjà décrits, et comporte de plus deux pattes radiales 112 qui sont orientées perpendiculairement à l'axe d'oscillation 34 défini par les bras radiaux 28, et qui s'étendent de la partie annulaire 26 vers la masse annulaire 30. Celle-ci comporte également deux pattes radiales 114, orientées vers la partie annulaire 26 depuis la surface cylindrique interne de la masse annulaire 30, les pattes radiales 112 et 114 étant alignées deux à deux et se terminant par des logements semi-cylindriques orientés l'un vers l'autre et dans lesquels sont logés des moyens tels que des goupilles élastiques 116 formant des moyens d'hystérésis pour l'amortissement des oscillations du volant d'inertie autour de l'axe 34. De façon plus générale, les moyens d'hystérésis comprennent des éléments intermédiaires montés entre la partie annulaire 26 et la masse annulaire 30, dans une direction perpendiculaire à l'axe 34. Dans le mode de réalisation de la figure 22, le volant flexible 10 comporte une partie annulaire radialement interne formée avec des orifices 24 de passage des moyens de fixation sur l'arbre menant et avec quatre bras radiaux 28 du type précité, qui sont orientés à 90 degrés les uns des autres et qui sont reliés à leurs extrémités radialement externes à la masse annulaire 30 par des languettes élastiquement déformables 120, 122 qui s'étendent dans un plan perpendiculaire à l'axe de rotation et qui sont fixées à leurs extrémités sur les bras radiaux 28 et sur la masse annulaire 30 par des vis, rivets ou analogues.In the embodiment of Figures 20 and 21, the flexible flywheel 10 is made in one piece and comprises a radially internal annular part 26 connected by two radial arms 28 diametrically opposite an annular mass 30, as in the modes of embodiment already described, and further comprises two radial lugs 112 which are oriented perpendicular to the axis of oscillation 34 defined by the radial arms 28, and which extend from the annular part 26 towards the annular mass 30. This this also includes two radial lugs 114, oriented towards the annular part 26 from the internal cylindrical surface of the annular mass 30, the radial lugs 112 and 114 being aligned in pairs and ending in semi-cylindrical housings oriented towards each other and in which are housed means such as elastic pins 116 forming hysteresis means for damping the oscillations of the flywheel around the axis 34. More generally, the hysteresis means comprise intermediate elements mounted between the part annular 26 and the annular mass 30, in a direction perpendicular to the axis 34. In the embodiment of FIG. 22, the flexible flywheel 10 comprises a radially internal annular part formed with orifices 24 for passage of the fixing means on the driving shaft and with four radial arms 28 of the aforementioned type, which are oriented 90 degrees from each other and which are connected at their ends radially ex dull to the annular mass 30 by elastically deformable tongues 120, 122 which extend in a plane perpendicular to the axis of rotation and which are fixed at their ends to the radial arms 28 and to the annular mass 30 by screws, rivets or the like.
Dans le mode de réalisation représenté, chaque languette 120, 122 est de forme allongée et s'étend dans une direction sensiblement perpendiculaire au bras radial 28 sur lequel elle est fixée.In the embodiment shown, each tongue 120, 122 is of elongated shape and extends in a direction substantially perpendicular to the radial arm 28 on which it is fixed.
On définit ainsi deux axes 34, 124 d'oscillation du volant flexible qui sont perpendiculaires à l'axe de rotation et perpendiculaires entre eux, l'un de ces axes d'oscillation correspondant à l'axe 34 précité et l'autre 124 lui étant perpendiculaire.Two axes 34, 124 of oscillation of the flexible flywheel are thus defined which are perpendicular to the axis of rotation and perpendicular to each other, one of these axes of oscillation corresponding to the above-mentioned axis 34 and the other 124 itself. being perpendicular.
Les languettes 120 fixées aux bras radiaux 28 définissant l'axe d'oscillation 124 ont une raideur inférieure à celle des languettes 122 fixées aux bras radiaux 28 définissant l'axe d'oscillation 34. Cela permet de disposer de deux fréquences d'oscillation autour de deux axes perpendiculaires qui sont chacun dans une position angulaire déterminée par rapport à l'arbre menant. L'oscillation autour de l'axe 34 est caractérisée par une faible raideur et donc par une faible fréquence, tandis que l'oscillation autour de l'axe 124 est caractérisée par une raideur plus importante et donc par une fréquence plus élevée. On peut parvenir au même résultat en disposant des masses différentes générant des inerties différentes sur les deux axes d'oscillation 34 et 124. Lorsque les masses disposées sur un axe d'oscillation sont plus grandes, la fréquence d'oscillation est plus faible autour de l'axe perpendiculaire à cet axe d'oscillation. On peut bien entendu combiner ces deux moyens, c'est-à-dire différencier les raideurs des languettes 120 et 122 et les masses disposées sur les axes d'oscillation.The tongues 120 fixed to the radial arms 28 defining the axis of oscillation 124 have a stiffness less than that of the tongues 122 fixed to the radial arms 28 defining the axis of oscillation 34. This makes it possible to have two frequencies of oscillation around of two perpendicular axes which are each in a determined angular position relative to the driving shaft. The oscillation around the axis 34 is characterized by a low stiffness and therefore by a low frequency, while the oscillation around the axis 124 is characterized by a greater stiffness and therefore by a higher frequency. The same result can be achieved by having different masses generating different inertias on the two oscillation axes 34 and 124. When the masses placed on an oscillation axis are larger, the oscillation frequency is lower around the axis perpendicular to this axis of oscillation. It is of course possible to combine these two means, that is to say to differentiate the stiffnesses of the tongues 120 and 122 and the masses disposed on the axes of oscillation.
On peut aussi, en variante, relier les bras 28 sur l'axe 124 par deux languettes 120 à la masse annulaire 30 et ne pas avoir de languettes 122, les languettes 120 aidant à la transmission du couple.One can also, as a variant, connect the arms 28 on the axis 124 by two tongues 120 to the annular mass 30 and not have tongues 122, the tongues 120 helping to transmit the torque.
Dans les modes de réalisation des figures 23 à 26, le volant d'inertie flexible selon l'invention fait partie d'un double volant amortisseur et forme le volant primaire de celui-ci.In the embodiments of FIGS. 23 to 26, the flexible flywheel according to the invention forms part of a double damping flywheel and forms the primary flywheel thereof.
En figure 23, le volant primaire flexible 10 comprend une partie annulaire radialement interne 26 formant moyeu, sur laquelle est fixée par des rivets 130 la partie radialement interne d'une tôle annulaire flexible 132 dont la périphérie radialement externe est fixée par serrage axial sur une masse annulaire 30 formée de deux bagues cylindriques 134, 136, soudées l'une à l'intérieur de l'autre, la périphérie externe de la tôle annulaire 132 étant serrée entre une extrémité axiale de la bague interne 134 et un rebord d'extrémité de la bague externe 136.In FIG. 23, the flexible primary flywheel 10 comprises a radially internal annular part 26 forming a hub, to which is fixed by rivets 130 the radially internal part of a flexible annular sheet 132 whose radially external periphery is fixed by axial clamping on a annular mass 30 formed of two cylindrical rings 134, 136, welded one inside the other, the external periphery of the annular sheet 132 being clamped between an axial end of the internal ring 134 and an end flange of the outer ring 136.
Des moyens d'hystérésis sont associés à cette tôle annulaire flexible et sont formés par une rondelle élastique 138 dont la périphérie radialement externe est serrée avec la périphérie radialement externe de la tôle annulaire 132 entre les bagues 134 et 136 comme indiqué, et dont la partie annulaire radialement interne comporte des pattes radiales 140 qui sont appliquées élastiquement sur la tôle annulaire flexible 132.Hysteresis means are associated with this flexible annular sheet and are formed by an elastic washer 138 whose radially outer periphery is clamped with the radially outer periphery of the annular sheet 132 between the rings 134 and 136 as indicated, and whose radially internal annular part comprises radial lugs 140 which are applied elastically to the flexible annular sheet 132.
Le volant primaire flexible 10 est associé à un volant secondaire 142 qui est centré et guidé en rotation sur le moyeu 26 au moyen d'un palier lisse 144 et qui forme le plateau de réaction d'un embrayage d'un type classique.The flexible primary flywheel 10 is associated with a secondary flywheel 142 which is centered and guided in rotation on the hub 26 by means of a plain bearing 144 and which forms the reaction plate of a clutch of a conventional type.
Un amortisseur de torsion 146 à ressorts circonférentiels est monté entre les deux volants d'inertie et les relie en rotation avec une possibilité de débattement angulaire entre eux, pour l'absorption des vibrations et irrégularités de couple.A torsional damper 146 with circumferential springs is mounted between the two flywheels and connects them in rotation with a possibility of angular movement between them, for the absorption of vibrations and torque irregularities.
Cet amortisseur de torsion comprend, de façon classique, un élément d'entrée qui est solidaire en rotation du volant primaire 10 et un élément de sortie qui est solidaire en rotation du volant secondaire 142, l'élément d'entrée étant ici fixé par des rivets 148 sur la rondelle élastique 138 tandis que l'élément de sortie est fixé par des rivets 150 sur le volant secondaire.This torsional damper conventionally comprises an input element which is integral in rotation with the primary flywheel 10 and an output element which is integral in rotation with the secondary flywheel 142, the input element here being fixed by rivets 148 on the elastic washer 138 while the outlet element is fixed by rivets 150 on the secondary flywheel.
Un limiteur de couple est formé par le montage à serrage axial de la périphérie externe de la tôle annulaire 132 entre les bagues 134 et 136 de la masse annulaire 30, ce serrage axial permettant une rotation relative de la tôle annulaire 132 par rapport à la rondelle élastique 138 lorsque le couple transmis est supérieur à une valeur maximale prédéterminée.A torque limiter is formed by the axially clamped mounting of the external periphery of the annular sheet 132 between the rings 134 and 136 of the annular mass 30, this axial clamping allowing relative rotation of the annular sheet 132 relative to the washer. elastic 138 when the transmitted torque is greater than a predetermined maximum value.
Dans la variante de réalisation représentée en figure 24, qui est une demi-vue en coupe axiale d'un volant primaire flexible pour double volant amortisseur, le volant primaire 10 comprend une tôle annulaire flexible 152 dont la partie radicalement interne est fixée au moyen de vis 154 sur l'extrémité de l'arbre menant en même temps qu'un moyeu cylindrique formant la partie annulaire interne 26 du volant flexible, et la partie annulaire radialement externe de cette tôle 152 est fixée par des rivets 156 sur une masse annulaire 30 en fonte. Cette masse annulaire 30 porte une couronne de démarreur ainsi qu'une tôle de fermeture 158 du côté opposé à l'arbre menant, cette tôle 158 étant fixée à la masse annulaire 30 par des rivets 160 et comportant un rebord périphérique interne 162 orienté radialement et disposé au voisinage de la tôle annulaire flexible 152.In the variant embodiment shown in FIG. 24, which is a half-view in axial section of a flexible primary flywheel for a double shock-absorbing flywheel, the primary flywheel 10 comprises a flexible annular sheet 152 whose radially internal part is fixed by means of screw 154 on the end of the shaft leading at the same time as a cylindrical hub forming the internal annular part 26 of the flexible flywheel, and the radially external annular part of this sheet 152 is fixed by rivets 156 on an annular mass 30 cast. This annular mass 30 carries a starter ring as well as a closing plate 158 on the side opposite to the driving shaft, this plate 158 being fixed to the annular mass 30 by rivets 160 and comprising an internal peripheral rim 162 oriented radially and disposed in the vicinity of the flexible annular sheet 152.
Une rondelle élastique 164 est montée entre la tôle annulaire flexible 152 et le rebord 162 de la tôle de fermeture 158 et forme des moyens d'hystérésis pour l'amortissement des vibrations en flexion du volant primaire 10.An elastic washer 164 is mounted between the flexible annular sheet 152 and the flange 162 of the closure sheet 158 and forms hysteresis means for damping the bending vibrations of the primary flywheel 10.
Dans les variantes de réalisation des figures 25 et 26, le double volant amortisseur représenté en coupe axiale comprend un volant primaire flexible 10 selon l'invention, un volant secondaire 170 formé de deux parties annulaires 172 et 174 reliées entre elles par un limiteur de couple 176, un roulement 178 de centrage et de guidage en rotation du volant secondaire 170 sur un moyeu cylindrique formé par la partie annulaire radialement interne 26 du volant primaire 10, et un amortisseur de torsion 180 qui est monté entre les deux volants d'inertie et qui est du type radial ou à ressorts radiaux.In the variant embodiments of FIGS. 25 and 26, the double damping flywheel shown in axial section comprises a flexible primary flywheel 10 according to the invention, a secondary flywheel 170 formed by two annular parts 172 and 174 connected together by a torque limiter 176, a bearing 178 for centering and guiding in rotation the secondary flywheel 170 on a cylindrical hub formed by the radially internal annular part 26 of the primary flywheel 10, and a torsion damper 180 which is mounted between the two flywheels and which is of the radial or radial spring type.
De façon connue, les ressorts 182 de cet amortisseur de torsion sont guidés sur des tiges cylindriques 184 logées dans des boîtes cylindriques 186, qui sont montées pivotantes à leurs extrémités radialement externes sur la masse annulaire 30 du volant primaire autour d'un axe 188 parallèle à l'axe de rotation, tandis que les extrémités radialement internes des tiges cylindriques 184 sont montées pivotantes sur la partie annulaire interne 174 du volant secondaire 170 au moyen d'axes 190 parallèles à l'axe de rotation. La masse annulaire 30 du volant primaire comporte des blocs 192 en fonte, logés entre les boîtes cylindriques 186 des ressorts de l'amortisseur de torsion et ayant une forme sensiblement triangulaire à sommet orienté vers l'axe de rotation pour permettre un débattement angulaire des boîtes cylindriques autour de leurs axes 188 d'articulation sur la masse annulaire 30. Les masses des blocs 192 peuvent être réparties sur les deux axes perpendiculaires d'oscillation 34 et 124, comme décrit en référence à la figure 22.In known manner, the springs 182 of this torsion damper are guided on cylindrical rods 184 housed in cylindrical boxes 186, which are pivotally mounted at their radially external ends on the annular mass 30 of the primary flywheel around a parallel axis 188 to the axis of rotation, while the radially internal ends of the cylindrical rods 184 are pivotally mounted on the internal annular part 174 of the secondary flywheel 170 by means of axes 190 parallel to the axis of rotation. The annular mass 30 of the primary flywheel comprises blocks 192 of cast iron, housed between the cylindrical boxes 186 of the springs of the torsion damper and having a substantially triangular shape with apex oriented towards the axis of rotation to allow angular movement of the boxes. cylindrical around their axes 188 of articulation on the annular mass 30. The masses of the blocks 192 can be distributed on the two perpendicular axes of oscillation 34 and 124, as described with reference to FIG. 22.
Les blocs 192 sont fixés par des rivets 194 sur une tôle 196 de la masse annulaire 30 du volant primaire, en même temps que la partie radialement externe de la tôle annulaire flexible 132 du volant primaire.The blocks 192 are fixed by rivets 194 to a sheet 196 of the annular mass 30 of the primary flywheel, at the same time as the radially external part of the flexible annular sheet 132 of the primary flywheel.
Une rondelle élastique 198 est montée entre la tôle annulaire 132 et un rebord radial 200 de la tôle 196 précitée, du côté du volant primaire tourné vers l'arbre menant. Cette rondelle élastique forme des moyens d'amortissement des vibrations en flexion du volant primaire.An elastic washer 198 is mounted between the annular sheet 132 and a radial flange 200 of the aforementioned sheet 196, on the side of the primary flywheel facing the driving shaft. This elastic washer forms means for damping the flexural vibrations of the primary flywheel.
Le mode de réalisation représenté en figure 26 ne diffère de celui de la figure 25 que par la constitution des blocs 192 portés par le volant primaire, qui sont ici constitués d'un empilement axial de tôles 202 fixées par les rivets 194 précités sur la tôle 196 du volant primaire, en même temps que la partie périphérique radialement externe de la tôle annulaire flexible 132.The embodiment shown in FIG. 26 differs from that of FIG. 25 only by the constitution of the blocks 192 carried by the primary flywheel, which here consist of an axial stack of sheets 202 fixed by the aforesaid rivets 194 on the sheet. 196 of the primary flywheel, at the same time as the radially external peripheral part of the flexible annular sheet 132.
Pour le reste, la structure est identique à celle déjà décrite en référence à la figure 25.For the rest, the structure is identical to that already described with reference to FIG. 25.
En référence à la figure 27, nous allons décrire maintenant plus en détails le positionnement d'un volant flexible selon l'invention sur l'arbre menant.Referring to Figure 27, we will now describe in more detail the positioning of a flexible flywheel according to the invention on the drive shaft.
L'arbre menant 12 est généralement un vilebrequin comportant au moins un maneton 1200,1201 apte à être relié à au moins une bielle (non représentée) associée à un piston d'un moteur thermique. Le maneton appelé premier maneton 1200 est adjacent au volant flexible 10 selon l'invention. Le maneton 1200 définit en association avec l'axe de rotation 22 de l'arbre menant et du volant flexible 10 un plan P. Comme nous l'avons vue précédemment, l'axe d'oscillation 34 du volant flexible 10 selon l'invention est sensiblement perpendiculaire à l'axe de rotation 22 et il est positionné angulairement par rapport à l'arbre menant 12. Cette position angulaire est déterminée entre le plan P précédemment décrit et l'axe d'oscillation 34 qui présentent alors un angle de positionnement α entre eux.The driving shaft 12 is generally a crankshaft comprising at least one crankpin 1200,1201 capable of being connected to at least one connecting rod (not shown) associated with a piston of a heat engine. The crank pin called first crank pin 1200 is adjacent to the flexible flywheel 10 according to the invention. The crankpin 1200 defines in association with the axis of rotation 22 of the driving shaft and the flexible flywheel 10 a plane P. As we have seen previously, the axis of oscillation 34 of the flexible flywheel 10 according to the invention is substantially perpendicular to the axis of rotation 22 and it is positioned angularly with respect to the driving shaft 12. This angular position is determined between the plane P previously described and the axis of oscillation 34 which then have a positioning angle α between them.
La valeur de l'angle de positionnement α est optimisée afin de permettre une réduction des contraintes dans l'arbre menant et/ou des bruits générés par le moteur. La détermination de la valeur de l'angle de positionnement α s'effectue par mesures ou bien par calcul. Cette valeur est fonction du nombre de cylindres du moteur thermique considéré ainsi que de la disposition desdits cylindres. Cette valeur est aussi fonction du ou des phénomènes dont une réduction est recherchée (essentiellement les contraintes et les bruits). D'autre part, la mesure de la valeur de l'angle de positionnement α s'effectue dans un sens de rotation R de l'arbre menant depuis le plan P à l'axe d'oscillation 34 du volant flexible 10 selon l'invention.The value of the positioning angle α is optimized in order to allow a reduction of the stresses in the driving shaft and / or of the noises generated by the motor. The value of the positioning angle α is determined by measurement or by calculation. This value is a function of the number of cylinders of the thermal engine considered as well as of the arrangement of said cylinders. This value is also a function of the phenomenon or phenomena for which a reduction is sought (essentially the constraints and the noises). On the other hand, the value of the positioning angle α is measured in a direction of rotation R of the shaft leading from the plane P to the axis of oscillation 34 of the flexible flywheel 10 along the invention.
Par exemple, lorsque l'axe d'oscillation 34 est proche d'une perpendiculaire au plan P (c'est-à-dire la valeur de l'angle de positionnement α est égale à environ 90°), cette position permet alors une réduction des contraintes dans le vilebrequin principalement.For example, when the axis of oscillation 34 is close to a perpendicular to the plane P (that is to say the value of the positioning angle α is equal to approximately 90 °), this position then allows a reduction of stresses in the crankshaft mainly.
II a été constaté que, dans un moteur thermique, la pression maximale exercée sur une tête de piston se situe alors que le maneton portant ledit piston fait un angle avec la verticale de l'ordre de 15° à 20° environ dans le sens de rotation, soit un angle sensiblement supérieur à l'angle dit d'explosion (angle avec la verticale que prend le maneton au moment de l'explosion). Un décalage dans le sens de rotation de l'arbre menant de l'ordre de 15° à 20 ° environ du volant flexible 10 selon l'invention permet de réduire les bruits.It has been observed that, in a heat engine, the maximum pressure exerted on a piston head is situated while the crank pin carrying said piston makes an angle with the vertical of the order of approximately 15 ° to 20 ° in the direction of rotation, that is to say an angle appreciably greater than the so-called explosion angle (angle with the vertical that the crank pin takes at the time of the explosion). An offset in the direction of rotation of the shaft leading on the order of approximately 15 ° to 20 ° of the flexible flywheel 10 according to the invention makes it possible to reduce noise.
Ainsi, la valeur de l'angle de positionnement α peut être comprise entre 80° environ et 120° environ. Cela permet de pondérer la réduction des bruits générés par rapport à la réduction des contraintes et inversement. De manière avantageuse, la valeur de l'angle de positionnement α peut être comprise entre environ 90° et 110° environs.Thus, the value of the positioning angle α can be between approximately 80 ° and approximately 120 °. This makes it possible to weight the reduction in noise generated compared to the reduction in stresses and vice versa. Advantageously, the value of the positioning angle α can be between approximately 90 ° and around 110 °.
Avantageusement, pour une valeur de l'angle de positionnement α d'environs 90°, les contraintes sont réduites, alors que pour une valeur de l'angle de positionnement α d'environ 110°, les bruits générés sont réduits.Advantageously, for a value of the positioning angle α of around 90 °, the stresses are reduced, while for a value of the positioning angle α of around 110 °, the noise generated is reduced.
Les valeurs intermédiaires de l'angle de positionnement α permettent d'adapter les réductions de contraintes et de bruits générés en fonction de ce qui est recherché dans cette matière. The intermediate values of the positioning angle α make it possible to adapt the stress and noise reductions generated as a function of what is sought in this material.

Claims

REVENDICATIONS
1) Volant d'inertie flexible pour dispositif de transmission de couple, en particulier pour véhicule automobile, destiné à être entraîné autour d'un axe de rotation (22), par un arbre menant (12) et comprenant une masse annulaire (30) portée par un élément flexible destiné à être fixé à l'arbre menant, caractérisé en ce que l'élément flexible comprend des bras radiaux (28) définissant un axe privilégié d'oscillation (34) perpendiculaire à l'axe de rotation (22) du volant.1) Flexible flywheel for torque transmission device, in particular for a motor vehicle, intended to be driven around an axis of rotation (22), by a driving shaft (12) and comprising an annular mass (30) carried by a flexible element intended to be fixed to the driving shaft, characterized in that the flexible element comprises radial arms (28) defining a privileged axis of oscillation (34) perpendicular to the axis of rotation (22) of the steering wheel.
2) Volant selon la revendication 1 , caractérisé en ce que l'axe d'oscillation (34) a une position angulaire prédéterminée par rapport à l'arbre menant (22).2) Steering wheel according to claim 1, characterized in that the oscillation axis (34) has a predetermined angular position relative to the driving shaft (22).
3) Volant selon la revendication 1 ou 2, caractérisé en ce que les bras radiaux (28) s'étendent entre l'axe de rotation (22) et la masse annulaire (30).3) Steering wheel according to claim 1 or 2, characterized in that the radial arms (28) extend between the axis of rotation (22) and the annular mass (30).
4) Volant selon l'une des revendications précédentes, caractérisé en ce que l'axe d'oscillation (34) est formé de deux bras radiaux s'étendant dans le prolongement l'un de l'autre, entre l'axe de rotation et la masse annulaire (30).4) Steering wheel according to one of the preceding claims, characterized in that the oscillation axis (34) is formed by two radial arms extending in extension of one another, between the axis of rotation and the annular mass (30).
5) Volant selon l'une des revendications 1 à 3, caractérisé en ce que l'axe d'oscillation (34) est formé par trois bras radiaux (28, 40) dont deux sont symétriques l'un de l'autre par rapport au prolongement du troisième bras radial (28). 6) Volant selon l'une des revendications précédentes, caractérisé en ce que ledit élément flexible est de forme annulaire et comporte des évidements (64) de part et d'autre de l'axe d'oscillation.5) Steering wheel according to one of claims 1 to 3, characterized in that the oscillation axis (34) is formed by three radial arms (28, 40), two of which are symmetrical with respect to one another to the extension of the third radial arm (28). 6) Steering wheel according to one of the preceding claims, characterized in that said flexible element is of annular shape and has recesses (64) on either side of the axis of oscillation.
7) Volant selon la revendication 6, caractérisé en ce que les évidements (64) sont traversants. 8) Volant selon l'une des revendications précédentes, caractérisé en ce que ledit élément flexible est formé d'une seule pièce avec la masse annulaire (30).7) Steering wheel according to claim 6, characterized in that the recesses (64) are through. 8) Steering wheel according to one of the preceding claims, characterized in that said flexible element is formed in one piece with the annular mass (30).
9) Volant selon l'une des revendications précédentes, caractérisé en ce que ledit élément flexible est en fonte.9) Steering wheel according to one of the preceding claims, characterized in that said flexible element is made of cast iron.
10) Volant selon l'une des revendications 1 à 8, caractérisé en ce que ledit élément flexible est en acier.10) Steering wheel according to one of claims 1 to 8, characterized in that said flexible element is made of steel.
11) Volant selon la revendication 10, caractérisé en ce que ledit élément flexible est une pièce séparée et est fixé sur la masse annulaire (30) par des vis (54, 82), des rivets ou analogues aux extrémités des bras radiaux précités.11) Steering wheel according to claim 10, characterized in that said flexible element is a separate piece and is fixed to the annular mass (30) by screws (54, 82), rivets or the like at the ends of the above-mentioned radial arms.
12) Volant selon la revendication 10 ou 11 , caractérisé en ce que ledit élément flexible est formé de plusieurs éléments plats (72) superposés et fixés ensemble sur la masse annulaire (30). 13) Volant selon l'une des revendications précédentes, caractérisé en ce que les bras radiaux (38) définissant l'axe d'oscillation (34) sont raccordés à leurs extrémités radialement internes à un anneau central (26), comportant des orifices (24) de passage de moyens de fixation sur l'arbre menant. 14) Volant selon l'une des revendications précédentes, caractérisé en ce qu'il comprend des moyens d'hystérésis (42, 100, 102, 110) portés par l'élément flexible et coopérant par frottement avec la masse annulaire (30).12) Steering wheel according to claim 10 or 11, characterized in that said flexible element is formed of several flat elements (72) superimposed and fixed together on the annular mass (30). 13) Steering wheel according to one of the preceding claims, characterized in that the radial arms (38) defining the oscillation axis (34) are connected at their radially internal ends to a central ring (26), comprising orifices ( 24) passage of fixing means on the driving shaft. 14) Steering wheel according to one of the preceding claims, characterized in that it comprises hysteresis means (42, 100, 102, 110) carried by the flexible element and cooperating by friction with the annular mass (30).
15) Volant selon la revendication 14, caractérisé en ce que les moyens d'hystérésis comprennent deux bras radiaux (42) s'étendant perpendiculairement à l'axe d'oscillation (34) et ayant des extrémités radialement internes solidaires de l'élément flexible et des extrémités radialement externes (48) en contact avec la masse annulaire (30).15) Steering wheel according to claim 14, characterized in that the hysteresis means comprise two radial arms (42) extending perpendicular to the axis of oscillation (34) and having radially internal ends integral with the flexible element and radially outer ends (48) in contact with the annular mass (30).
16) Volant selon la revendication 15, caractérisé en ce que les bras radiaux des moyens d'hystérésis font partie de l'élément flexible. 17) Volant selon la revendication 16, caractérisé en ce que l'élément flexible (72) comprend un empilement d'éléments plats et les bras radiaux (100) des moyens d'hystérésis sont formés sur un élément (96) de cet empilement. 18) Volant selon la revendication 15, caractérisé en ce les bras radiaux des moyens d'hystérésis font partie d'une rondelle (42) rapportée sur l'élément flexible.16) Steering wheel according to claim 15, characterized in that the radial arms of the hysteresis means are part of the flexible element. 17) Steering wheel according to claim 16, characterized in that the flexible element (72) comprises a stack of flat elements and the radial arms (100) of the hysteresis means are formed on an element (96) of this stack. 18) Steering wheel according to claim 15, characterized in that the radial arms of the hysteresis means are part of a washer (42) attached to the flexible element.
19) Volant selon la revendication 18, caractérisé en ce que ladite rondelle (42) est destinée à être fixée avec l'élément flexible sur l'arbre menant.19) Steering wheel according to claim 18, characterized in that said washer (42) is intended to be fixed with the flexible element on the driving shaft.
20) Volant selon la revendication 14, caractérisé en ce que les moyens d'hystérésis comprennent des éléments intermédiaires montés entre la masse annulaire (30) et une partie annulaire interne (26) de l'élément flexible, dans une direction perpendiculaire à l'axe privilégié (34). 21) Volant selon la revendication 14, caractérisé en ce que les moyens d'hystérésis comprennent des goupilles élastiques (116) montées dans des logements semi-cylindriques de deux pattes (112) solidaires de l'élément flexible et de deux pattes (144) solidaires de la masse annulaire (30), lesdites pattes s'étendant dans une direction perpendiculaire à l'axe d'oscillation (34).20) Steering wheel according to claim 14, characterized in that the hysteresis means comprise intermediate elements mounted between the annular mass (30) and an internal annular part (26) of the flexible element, in a direction perpendicular to the privileged axis (34). 21) Steering wheel according to claim 14, characterized in that the hysteresis means comprise elastic pins (116) mounted in semi-cylindrical housings of two legs (112) integral with the flexible element and two legs (144) integral with the annular mass (30), said tabs extending in a direction perpendicular to the axis of oscillation (34).
22) Volant selon l'une des revendications précédentes, caractérisé en ce que les bras radiaux (78) définissant l'axe d'oscillation comportent, entre leurs extrémités radialement internes et radialement externes, des découpes ou encoches (84) de localisation de contraintes maximales.22) Steering wheel according to one of the preceding claims, characterized in that the radial arms (78) defining the axis of oscillation comprise, between their radially internal and radially external ends, cutouts or notches (84) for locating stresses maximum.
23) Volant selon l'une des revendications précédentes, caractérisé en ce que les bras radiaux (28) définissant l'axe d'oscillation (34) sont légèrement inclinés en oblique par rapport à une perpendiculaire à l'axe de rotation dans une direction opposée à l'arbre menant à partir de leur extrémité radialement interne. 24) Volant selon l'une des revendications précédentes, caractérisé en ce que ledit élément flexible comprend des moyens (28) définissant un second axe d'oscillation (124) perpendiculaire à l'axe de rotation (22) et à l'axe privilégié d'oscillation (34), le second axe d'oscillation (124) ayant une raideur supérieure à celle de l'axe privilégié (34).23) Steering wheel according to one of the preceding claims, characterized in that the radial arms (28) defining the axis of oscillation (34) are slightly inclined obliquely relative to a perpendicular to the axis of rotation in a direction opposite the shaft leading from their radially inner end. 24) Steering wheel according to one of the preceding claims, characterized in that said flexible element comprises means (28) defining a second axis of oscillation (124) perpendicular to the axis of rotation (22) and to the preferred axis of oscillation (34), the second axis of oscillation (124) having a stiffness greater than that of the preferred axis (34).
25) Volant selon la revendication 24, caractérisé en ce que les deux axes d'oscillation (34, 124) sont définis par des bras radiaux (28) de l'élément flexible. 26) Volant selon la revendication 25, caractérisé en ce que lesdits bras radiaux (28) sont reliés à la masse annulaire (30) par des languettes (120, 122).25) Steering wheel according to claim 24, characterized in that the two axes of oscillation (34, 124) are defined by radial arms (28) of the flexible element. 26) Steering wheel according to claim 25, characterized in that said radial arms (28) are connected to the annular mass (30) by tongues (120, 122).
27) Volant selon la revendication 26, caractérisé en ce que les languettes (120) reliant deux bras radiaux alignés à la masse annulaire (30) ont une raideur différente de celle des languettes (122) reliant les deux autres bras radiaux 28 à la masse annulaire (30).27) Steering wheel according to claim 26, characterized in that the tongues (120) connecting two radial arms aligned with the annular mass (30) have a stiffness different from that of the tongues (122) connecting the other two radial arms 28 to the mass annular (30).
28) Volant selon l'une des revendications précédentes, caractérisé en ce qu'il forme le volant primaire d'un double volant amortisseur comprenant également un volant secondaire (142, 170) destiné à être relié à l'arbre d'entrée d'une transmission et un amortisseur de torsion (146, 180) monté entre les deux volants.28) Steering wheel according to one of the preceding claims, characterized in that it forms the primary flywheel of a double damping flywheel also comprising a secondary flywheel (142, 170) intended to be connected to the input shaft of a transmission and a torsional damper (146, 180) mounted between the two flywheels.
29) Volant selon la revendication 28, caractérisé en ce que l'amortisseur de torsion (180) est du type comprenant des ressorts (182) orientés radialement au repos. 29) Steering wheel according to claim 28, characterized in that the torsion damper (180) is of the type comprising springs (182) oriented radially at rest.
EP04700270A 2003-01-06 2004-01-06 Flexible flywheel for torque transmission device Withdrawn EP1581752A2 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0300063A FR2849683B1 (en) 2003-01-06 2003-01-06 FLEXIBLE INERTILE WHEEL FOR TORQUE TRANSMISSION DEVICE
FR0300063 2003-01-06
PCT/FR2004/050002 WO2004065807A2 (en) 2003-01-06 2004-01-06 Flexible flywheel for torque transmission device

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EP1581752A2 true EP1581752A2 (en) 2005-10-05

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KR (1) KR101087884B1 (en)
BR (1) BRPI0406461A (en)
DE (1) DE112004000107T5 (en)
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WO (1) WO2004065807A2 (en)

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FR2883943B1 (en) 2005-04-04 2009-02-13 Renault Sas FLYWHEEL INERTIA ENGINE AJOURE
FR2890716B1 (en) 2005-09-09 2007-12-07 Valeo Embrayages FLEXIBLE INERTIAL WHEEL, ESPECIALLY FOR A MOTOR VEHICLE
FR2895479B1 (en) * 2005-12-27 2012-03-23 Renault Sas FLYWHEEL COMPRISING MEANS FOR DAMPING THE OSCILLATIONS OF SAID ENGINE FLYWHEEL
FR2895471B1 (en) * 2005-12-27 2009-05-22 Renault Sas TORQUE TRANSMISSION DEVICE COMPRISING A STEERING WHEEL AND DAMPING MEANS FOR SWING OF THE ENGINE FLYWHEEL
FR2899661B1 (en) * 2006-04-06 2008-06-13 Valeo Embrayages TORQUE LIMITER
DE102007008834A1 (en) * 2006-12-18 2008-06-19 Borgwarner Inc.(N.D.Ges.D.Staates Delaware), Auburn Hills Torsional vibration damper with multipart primary element
FR2920507B1 (en) * 2007-08-29 2009-12-11 Valeo Embrayages FLEXIBLE WHEEL.
CN103280914B (en) * 2013-04-23 2016-04-20 中国科学院电工研究所 A kind of speedup or constant speed release the flywheel of energy
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FR3051524B1 (en) * 2016-05-20 2018-06-15 Peugeot Citroen Automobiles Sa WHEEL OF INERTIA
DE112020001446T5 (en) * 2019-03-25 2021-12-02 Aisin Takaoka Co., Ltd. FLEXIBLE FLYWHEEL
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WO2004065807A3 (en) 2004-11-11
KR20050086957A (en) 2005-08-30
FR2849683A1 (en) 2004-07-09
JP4724110B2 (en) 2011-07-13
KR101087884B1 (en) 2011-11-30
BRPI0406461A (en) 2005-12-06
FR2849683B1 (en) 2006-07-28
WO2004065807A2 (en) 2004-08-05
DE112004000107T5 (en) 2005-12-22
JP2006515048A (en) 2006-05-18

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