• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The invention relates to a torsion damper comprising: - a first element and a second element movable in rotation about an axis X, and - a blade damping means (9) for transmitting a torque and damping the rotational acyclisms between the first element and the second element, the blade damping means comprising: ○ a first and a second blade (9a, 9b) integral with the first element, ○ a first support member (11a) carried by the second element and in which: - for a rotation in a first direction of rotation (21), a bending of the first blade (9a) produces on the first support member (11a) the first restoring force, - for a relative rotation in the second direction of rotation (24) opposite the first direction of rotation, a bending of the second blade (9b) produces the second restoring force on the first support member.
    公开号:FR3033857A1
    申请号:FR1552113
    申请日:2015-03-16
    公开日:2016-09-23
    发明作者:Karthik Krishnasamy
    申请人:Valeo Embrayages SAS；
    IPC主号:
    专利说明:

    [0001] TECHNICAL FIELD OF THE INVENTION The invention relates to the field of transmissions for a motor vehicle and relates more particularly to a double damping flywheel.
    [0002] STATE OF THE ART In the field of automobile transmissions, it is known to provide torque transmission devices with torsion dampers for absorbing and damping the vibrations and acyclisms generated by an internal combustion engine.
    [0003] The torsion dampers comprise an input member and an output member rotatable about a common axis of rotation and resilient damping means for transmitting the torque and damping rotational acyclisms between the input member. and the output element. Such torsion dampers equip including double damping flywheels (DVA) and / or friction clutch, in the case of a manual or robotic transmission, or locking clutches, also called "lock-up" clutches, equipping hydraulic coupling devices, in the case of an automatic transmission. Document FR3000155 illustrates a torsion damper having resilient damping means formed of two resilient blades mounted on the input member and each cooperating with a respective cam follower mounted on the output member. The blades and cam followers are arranged such that, for angular displacement between the input member and the output member, on either side of a relative angular position of rest, the follower The cam moves along the blade and, in doing so, exerts a bending force on the resilient blade. By reaction, the resilient blade exerts on the cam follower a restoring force which tends to return the input and output elements to their angular rest position. The bending of the resilient blade thus makes it possible to damp the vibrations and the irregularities of rotation between the input element and the output element while ensuring the transmission of torque. However, the portions of the blades subjected to the bending forces caused by the cam follower are stressed and subjected to significant stresses regardless of the relative direction of rotation between the input and output elements, that is to say that a driving torque is transmitted from the primary flywheel to the secondary flywheel or a resistant torque is transmitted from the secondary flywheel to the primary flywheel. Moreover, in view of this arrangement, the characteristic curves of the transmission of the torque as a function of the deflection in the forward and backward directions can not be completely uncorrelated so that certain complex curves of transmission of the torque as a function of the angular deflection do not occur. can be realized. SUMMARY An aspect of the invention is based on the idea of solving the disadvantages of the prior art by providing a particularly effective torsion damper. According to one embodiment, the invention provides a torsion damper for a torque transmission device comprising: a first element and a second element that are rotatable relative to one another about an axis of rotation X and a blade damping means adapted to transmit rotational torque between the first member and the second member and damping rotational acyclisms between the first member and the second member; the blade damping means comprising: a first elastically deformable blade and a second elastically deformable blade, the first blade and the second blade being integral in rotation with the first element, and a first support member carried by the second element in which the first support member, the first blade and the second blade are arranged such that: - the first support member cooperates with the first blade by bending it to transmit a torque of the second element to the first element, and - the first support member cooperates with the second blade by bending to transmit a torque of the first element to the second element.
    [0004] The damper according to the invention thus makes it possible to prevent the same support member from urging the same blade to alternately transmit a torque from the first element to the second element and from the second element to the first element. The damper according to the invention thus makes it possible to avoid the biasing of the same blade portion to transmit alternately a torque from the first element to the second element and from the second element to the first element. This system makes it possible to reduce blade fatigue. of the torsion damper. In particular, the transmission of a torque in a first direction impacts a portion of the blade different from the portion of blade biased during the transmission of a torque in the opposite direction.
    [0005] The torsion damper also makes it possible to transmit a torque with an acceptable stress. The system of two separate blades biased according to the direction of transmission of the torque thus makes it possible to increase the length of the blades and thus to reduce the stresses on each of the blades. On the other hand, the damper also provides a wider variety of torque transmission curves because the blade portions biased for each direction of torque transmission are disjoint. According to other advantageous embodiments, such a system may have one or more of the following characteristics: the first support member, the first blade and the second blade are arranged in such a way that the first support member cooperates only with the first blade when a torque is transmitted from the second element to the first element and only with the second blade when a torque is transmitted from the first element to the second element. the first support member, the first blade and the second blade are arranged in such a way that at least a portion of the torque is transmitted by the first blade regardless of the value of a torque transmitted from the second element to the first element; and that at least a portion of the torque is transmitted by the second blade irrespective of the value of a torque transmitted from the first element to the second element. - For the entire range of operation of the damper, the first support member cooperates with at least one of the first and second blades. 5 - the first support member is simultaneously in contact with the first blade and with the second blade in the angular position of rest. the blade damping means is arranged such that, for a transmission of a torque from the second element to the first element, a relative rotation in a first direction of rotation between the first and second elements from an angular position resting occurs and the blade damping means exerts a first restoring force for biasing the first and second members toward their angular rest position, and for transmitting a torque from the first member to the second member, a relative rotation in a second direction of rotation opposite to the first direction of rotation between the first and second elements from the angular rest position is made and the blade damping means exerts a second return force to recall the first and second elements towards their angular position of rest; the first support member, the first blade and the second blade being arranged such that: o for a relative rotation in the first direction of rotation between the first and second elements from the angular position of rest, the first member the support cooperates with the first blade and exerts a bending force on said first blade, the bending of the first blade producing on the first support member the first restoring force, o for a relative rotation in the second direction of rotation opposite to the first direction of rotation between the first and second members from the angular position of rest, the first support member exerts a bending force on the second blade, the bending of the second blade producing on the first support member the second restoring force. each blade comprises: a first elastically deformable section, a second elastically deformable section, a fixing section fixed with respect to the first element, and wherein the damper further comprises a second support member carried by the second element, the first support member, the second support member, the first blade and the second blade being arranged such that: 5 o the first support member cooperates with the first deformable section of the first blade by bending it and the second bearing member cooperates with the second deformable section of the second blade by bending it to transmit a torque from the second member to the first member, and 10 o the second bearing member cooperates with the second member deformable section of the first blade by bending and the first support member cooperates with the first deformable section of the second blade by bending to transmit a co uple of the first element to the second element. The first and second blades are arranged such that: for a relative rotation in the first direction of rotation between the first and second elements from the angular position of rest, the first support member exerts a bending force on the first deformable section of the first blade and the second support member 20 exerts a bending force on the second deformable section of the second blade, the bending of the first deformable section of the first blade and the bending of the second deformable section of the second blade jointly producing the first biasing force, o for a relative rotation in the second direction of rotation between the first and second elements from the angular position from the angular position of rest, the second support member exerts a force bending on the second deformable section of the first blade and the first bearing member exerts a bending on the first deformable section of the dry blade wave, bending the second deformable section of the first blade and bending the first deformable section of the second blade jointly forming the second biasing force. - The damper further comprises an end stop so as to limit the relative rotation between the first element and the second element. The damper further comprises: a third and a fourth elastically deformable blades integral in rotation with the first element, a second support member carried by the second element, in which the second support member, the second element, third blade and the fourth blade are arranged such that: o for a relative rotation in the first direction of rotation between the first and second elements from the angular position of rest, the second support member cooperates with the third blade and exerts a bending stress on said third blade, the first restoring force being produced jointly by bending the first and third blades respectively on the first bearing member and the second bearing member, o for relative rotation according to the second direction of rotation opposite to the first direction of rotation between the first and second elements from the angular position from the angular position of rest, the second The bearing member exerts a bending force on the fourth blade, the second biasing force being produced jointly by bending the second and fourth blades respectively on the first bearing member and the second bearing member. each blade comprises: a first elastically deformable section; a second elastically deformable section; a fixed attachment section with respect to the first element; and the damper further comprises a second support member carried by the second element; first support member being arranged to cooperate with the first deformable section of the first and second blades, the second support member being arranged to cooperate with the second deformable section of the first and second blades, the first and second support members and the first and second blades being arranged such that: o for a relative rotation in the first direction of rotation between the first and second elements from the angular position of rest, the first support member exerts a bending force on the first deformable section 30 of the first blade and the second support member exerts a bending force on the second deformable section of the second blade, the bending of the first deformable section of the first blade and the bending of the second section of the second blade 5 jointly producing the first restoring force, o for a relative rotation in the second direction of rotation between the first and second second elements from the angular position of rest, the second support member exerts a bending force on the second deformable section of the first blade and the first support member 10 exerts a bending on the first deformable section of the second blade, flexing the second deformable section of the first blade and flexing the first section of the second blade together forming the second biasing force. the fixing section of each blade is situated between the first deformable section and the second deformable section of said blade. each blade has an axis of symmetry, a projection of the first blade in a plane perpendicular to the axis of rotation X being symmetrical to a projection of the second blade in said plane perpendicular to the axis of rotation X with respect to the X-axis of rotation - alternatively each blade has an axis of symmetry, a projection of the first blade in a plane perpendicular to the axis of rotation X being asymmetrical to a projection of the second blade in said plane perpendicular to the X axis of rotation relative to the axis of rotation X. - Each blade is asymmetrical, a projection of the first blade in a plane perpendicular to the axis of rotation X being symmetrical to a projection of the second blade in said plane perpendicular to the axis of rotation X with respect to the axis of rotation X - the first and second blades are fixed independently of one another on the first element. The first blade and the second blade are stacked axially. the first blade is fixed on the first element in axial support against the said first element, the torsion damper further comprising a spacer, the second blade being fixed on the first element bearing axially against the spacer, the spacer being axially interposed between the second blade and the first element, a portion of the first blade and a portion of the second blade being axially superimposed. each blade is fixed on the first element by two rivets. each first and second blade has a cam surface, and the first bearing member has a cam follower arranged to cooperate with the cam surface of the first blade to transmit a torque from the second member to the first member and to the first member. cam surface of the second blade for transmitting a torque from the first member to the second member. The cam follower is a roller rotatably mounted on the second element by means of a rolling bearing. the first support member is arranged radially outside the first and second resilient blades. Such an arrangement makes it possible to retain the elastic blade radially when it is subjected to centrifugal force. The elastic blade is arranged to deform in a plane perpendicular to the axis of rotation. BRIEF DESCRIPTION OF THE DRAWINGS The invention will be better understood, and other objects, details, features and advantages thereof will become more clearly apparent from the following description of several particular embodiments of the invention, given solely to illustrative and nonlimiting, with reference to the accompanying figures. In these figures: - Figure 1 is a schematic perspective view of a double damping flywheel in the assembled state; FIG. 2 is a diagrammatic perspective view of the double damping flywheel of FIG. 1 in which the secondary flywheel is partially shown so as to display the means for fixing the blades; - Figure 3 is a schematic representation of the blades and cam followers in a rest position of the double damping flywheel. FIG. 4 is a front view of a double damping flywheel of FIG. 1 represented in an angular displacement position of the flywheels in a direct direction with respect to their rest position and in which the secondary flywheel is is not shown to view the blades; - Figure 5 is a front view of a double damping flywheel of Figure 1 shown in a maximum angular displacement position of the flywheels 5 in a direct direction relative to their rest position in which the secondary flywheel is not shown to view the blades; FIG. 6 is a front view of the double damping flywheel of FIG. 1 shown in a position of maximum angular displacement in a retro direction and in which the secondary flywheel is not shown in order to view the blades; - Figure 7 is a front view of a double damping flywheel according to another embodiment shown in a rest position and wherein the secondary flywheel is not shown to view the blades; FIG. 8 is a front view of the double damping flywheel of FIG. 7 represented in a position of maximum angular displacement in the direct direction between the primary flywheel and the secondary flywheel and in which the secondary flywheel is not shown so to visualize the blades; FIG. 9 is a front view of the double damping flywheel of FIG. 7 shown in a maximum retro-angle angular displacement position exhibiting a maximum relative rotation in the second direction of rotation between the primary flywheel and the secondary flywheel, and wherein the secondary flywheel is not shown to view the blades. DETAILED DESCRIPTION OF EMBODIMENTS In the description and the claims, the terms "external" and "internal" as well as the "axial" and "radial" orientations will be used to designate, according to the definitions given in the description, elements of the torsion damper. By convention, the "radial" orientation is directed orthogonally to the X axis of rotation of the elements of the torsion damper determining the "axial" orientation and, from the inside towards the outside, away from said axis . The "circumferential" orientation is directed orthogonally to the X axis of rotation of the torsion damper and orthogonal to the radial direction. Thus, an element described as circumferentially developing is an element whose component develops in a circumferential direction. The terms "external" and "internal" 3033857 are used to define the relative position of one element with respect to another, with reference to the axis of rotation X of the damper, an element close to the axis is thus described as internal as opposed to an external element located radially at the periphery.
    [0006] The description below is for illustrative purposes in the context of a double damping flywheel. However, the invention applies to any torsion damper intended to be disposed in the transmission chain of a motor vehicle, between the internal combustion engine and the gearbox. Such a torsion damper can be integrated with numerous torque transmission devices such as a double damping flywheel, a hydraulic clutch coupling clutch, or a clutch friction. For the purposes of the present description and of the claims, the term "first element" may designate a torque input element of a shock absorber, such as a primary flywheel of a double damping flywheel and the term "second element". A torque output member, such as a secondary flywheel of a double damping flywheel, or vice versa. Figure 1 shows a schematic perspective view of a double damping flywheel 1 in the assembled state. A double damping flywheel 1 comprises a primary flywheel 2, intended to be fixed at the end of a crankshaft of an internal combustion engine, not shown, and a secondary flywheel 3 which is centered and guided on the primary flywheel 2 by means of a ball bearing. The secondary flywheel 3 is intended to form the reaction plate for a clutch, not shown, ensuring the transmission of torque to the input shaft of a gearbox. The flywheels of primary inertia 2 and secondary 3 are movably mounted about an axis of rotation X and are furthermore movable in rotation relative to each other about said axis X. The primary flywheel 2 comprises a radially inner hub supporting the ball rolling bearing which cooperates with an inner hub of the secondary flywheel 3.
    [0007] Holes for the passage of fixing screws are provided on the primary flywheel 2 and on the secondary flywheel 3 in order to allow the attachment of the primary flywheel 2 to the crankshaft of the engine. The secondary flywheel 3 also has passages for fixing a damping means on the secondary flywheel 3 by means of fastening means 4 such as rivets. The primary flywheel 2 carries, on its outer periphery, a ring gear 5 for driving in rotation of the primary flywheel 2 with a starter.
    [0008] The secondary flywheel 3 has a flat annular surface 6, facing away from the primary flywheel 2, forming a bearing surface for a friction lining of a clutch disc (not shown). The secondary flywheel 3 comprises, close to its outer edge, pads 7 and orifices 8 for mounting a clutch cover.
    [0009] The primary and secondary flywheels 3 are coupled in rotation by a damping means which makes it possible to transmit a torque and to dampen the rotation acyclisms between the primary and secondary flywheels 3 in order to reduce the vibrations coming from the engine. The damping means is adapted to transmit a driving torque from the primary flywheel to the secondary flywheel and a resistant torque of the secondary flywheel to the primary flywheel. The transmission of a driving torque from the primary flywheel to the secondary flywheel causes relative rotation of the primary flywheel relative to the secondary flywheel from the angular position of rest in a direct direction of rotation, while the transmission of a resistant torque causes a relative rotation of the primary flywheel relative to the secondary flywheel from the angular position of rest in a direction of retro rotation. In FIGS. 3 to 9, below, the arrows 24, 124 represent the relative rotation in the direct direction of the primary flywheel with respect to the secondary flywheel from the angular position of rest while the arrows 21, 121 represent the relative rotation according to the retro direction of the primary flywheel relative to the secondary flywheel from the angular position of rest. The damping means is an elastic means which exerts between the primary flywheel and the secondary flywheel a return force which tends to bring the flywheels of primary and secondary inertia to their angular position of rest. The damping means thus makes it possible to damp the vibrations and irregularities of rotation between the flywheels of primary and secondary inertia while ensuring the transmission of the torque. FIG. 2 represents a schematic perspective view of the double damping flywheel 1 of FIG. 1 in which the secondary flywheel 3 is partially shown so as to display the attachment of elastic blades 9 of a damping means on the secondary flywheel 3. In the embodiment shown in FIGS. 2 to 9, this damping means comprises two resilient blades 9 mounted integral in rotation with the secondary flywheel 3. Each blade 9 is fastened to the secondary flywheel by means of rivets 4. An attachment section of each blade is arranged to remain rigid and does not cooperate with the cam followers 11 which will be described later. The blades 9 are axially superimposed. A first blade 9a is fixed directly in contact with the secondary flywheel 3. A second blade 9b is fixed on the secondary flywheel 3 by means of a spacer 10. This spacer 10 is interposed axially between the secondary flywheel 3 and the second blade 9b. The spacer 10 has an axial thickness substantially equal to the thickness of the first blade 9a. The thickness of the spacer 10 avoids excessive friction between the first blade 9a and the second blade 9b during bending of the blades 9. The fastening rivets 4 of the first blade 9a are symmetrical to the fastening rivets 4 of the second blade 9b with respect to the axis of rotation X of the torsion damper 1. FIG. 3 schematically shows the blades 9 cooperating with cam followers 11. The blades 9 and the cam followers 11 of FIG. 3 are shown in a rest position of the double damping flywheel 1. The rest position of the double damping flywheel 1 corresponds to an equilibrium position taken by the flywheels when no torque is transmitted between the primary and secondary flywheels.
    [0010] The first blade 9a has the general shape of a crescent moon or horseshoe. The first blade 9a comprises, from a first end 12 to a second end 13, a first arcuate portion 14, a fixing portion 15 and a second arcuate portion 16. The first blade 9a may, as desired, be made of in one piece or be composed of a plurality of lamellae 30 arranged axially against each other.
    [0011] The fixing portion 15 has two through-passages 17 intended to cooperate with the rivets 4 to ensure the attachment of the first blade 9a to the secondary flywheel 3. The radius of curvature of the first arcuate portion 14 and the 5 length of this first arcuate portion 14 are determined according to the desired stiffness characteristic of the first blade 9a. The first arcuate portion 14 extends substantially circumferentially from the attachment portion 15 to the first end 12. The first arcuate portion 14 has an increasing radial dimension from the first end 12 to the attachment portion 15 The first blade 9a is symmetrical with respect to an axis 22 perpendicular to the axis of rotation X and passing through the axis of rotation X. In the illustrated embodiment, this axis of symmetry 22 passes in the center of the portion of fixing the first blade 9a, between the first arcuate portion 14 and the second arcuate portion 16. Thus, the second arcuate portion 16 has a shape similar to that of the first arcuate portion 14. The first arcuate portion 14 has a face radially outer a cam surface 18. This cam surface 18 cooperates with a first cam follower 11a. The cam surface 18 develops from the first end 12 to a rest area 19 of the radially outer face of the first arcuate portion 14. The rest area 19 corresponds to the area of the first arcuate portion 14 against which the first cam follower 11a bears when the double damping flywheel 1 is in the rest position. The first cam follower 1a is carried by the primary flywheel 2. The first cam follower 11a here is a roller 20 rotatably mounted on the primary flywheel 2. The first cam follower 11a is held in abutment against the surface 18. The roller 20 is arranged to roll against the cam surface 18 during a relative movement between the primary flywheels 2 and secondary 3 in the forward direction 24. The first cam follower 1 la is arranged radially at 30 l. outside the first arcuate portion 14 so as to radially maintain the first arcuate portion 14 when subjected to centrifugal force.
    [0012] The cam surface 18 is arranged such that, for a relative rotation between the primary flywheel 2 and the secondary flywheel 3 in the forward direction 24 from the rest position as shown in FIG. 3, the first follower of cam 11a moves on the cam surface 18 exerting a bending force on the first arcuate portion 14. By reaction, the first arcuate portion 14 exerts on the first cam follower 11a a restoring force having a circumferential component which tends to to return the primary flywheels 2 and secondary 3 to the rest position. Thus, the first arcuate portion 14 is capable of transmitting a driving torque from the primary flywheel 2 to the secondary flywheel 3.
    [0013] In addition, the torsional vibrations and the irregularities of torque which are produced by the engine and transmitted by the crankshaft to the primary flywheel 2 are damped by the bending of the first arcuate portion 14. The second arcuate portion 16 has a cam surface 23. During relative rotation between the primary flywheel 2 and the secondary flywheel 3 from the angular position of rest in the retro direction 21, the cam surface 23 cooperates with a second cam follower 11b. The second cam follower 11a is symmetrical to the first cam follower 11a with respect to the axis of rotation X. The cooperation between the cam surface 23 and the second cam follower 11b during relative rotation between the primary flywheel 2 and the secondary flywheel 3 in the retro direction 21 is similar to the cooperation between the cam surface 18 of the first arcuate portion 14 and the first cam follower 11a during a relative rotation between the primary flywheel 2 and the secondary flywheel 3 in the forward direction 24. In addition, the first blade 9a and the second blade 9b shown in Figure 3 have a similar shape. However, the first blade 9a and the second blade 9b are attached to the secondary flywheel 3 in opposite orientations. More particularly, there is a symmetry of the blades relative to each other when they are projected in a plane orthogonal to the axis X. On the one hand, the projection of the first blade 9a in a perpendicular plane the axis of rotation X is symmetrical about the axis of rotation X 30 to the projection of the second blade 9b in the same plane perpendicular to the axis of rotation X. This allows to balance the damper.
    [0014] On the other hand, in the embodiment illustrated in Figures 2 to 6, the first blade 9a and the second blade 9b are also symmetrical in projection in a plane perpendicular to the axis of rotation X, with respect to a plane parallel to the axis of rotation X and passing through the positions taken by the cam followers in 5 angular position of rest. This allows symmetrical depreciation live and retro. Due to the opposite orientation between the first blade 9a and the second blade 9b, a first arcuate portion 25 of the second blade 9b cooperates with the first cam follower 11a during a relative rotation between the primary flywheel 2 and 10 the secondary flywheel 3 in the retro direction 21 and a second arcuate portion 26 of the second blade 9b cooperates with the second cam follower 11b during a relative rotation between the primary flywheel 2 and the secondary flywheel 3 in the forward direction 24 The cooperation between the arcuate portions 25 and 26 of the second blade 9b and the first and second cam followers 11a and 11b is analogous to the cooperation between the arcuate portions 14 and 16 of the first blade 9a and the first and second cam followers 14a and 11b. the second cam follower 11a and 11b. Thus, a relative rotation between the primary flywheel 2 and the secondary flywheel 3 in the forward direction 24 from the rest position causes the first cam follower 11a to cooperate with the cam surface 18 of the first arcuate portion 14 of the first blade 9a and, simultaneously, the engagement of the second cam follower 11b with a cam surface 27 of the second arcuate portion 26 of the second blade 9b. Likewise, a relative rotation between the primary flywheel 2 and the secondary flywheel 3 in the retro direction 21 from the rest position causes the second cam follower 11b to cooperate with the cam surface 23 of the second arcuate portion 16 of the first 9a blade and, simultaneously, the cooperation of the first cam follower 11a with a cam surface 28 of the first arcuate portion 25 of the second blade 9b. As described above, the cooperation between the cam followers 11 and the blades 9 exerts a force able to return the primary flywheels 2 and secondary 3 to the rest position.
    [0015] Furthermore, by symmetry of the blades 9 in projection relative to the plane described above, the cam surfaces of the blades are of identical circumferential length in the embodiments illustrated in Figures 2 to 6.
    [0016] In a preferred embodiment illustrated in FIG. 3, in the rest position of the double damping flywheel 1, the first cam follower 11a is in simultaneous contact with the first arcuate portion 14 and 25 respectively of the first blade 9a and of FIG. the second blade 9b. Similarly, in this rest position, the second cam follower 11b is in simultaneous contact with the second arcuate portion 16 and 26 respectively of the first blade 9a and the second blade 9b. According to an advantageous embodiment, the radii of curvature and the stiffness of the arcuate portions are such that, in the rest position, each cam follower 11 is located at the end of the cam surfaces of the two arcuate portions with which it cooperates. Thus, during a relative rotation between the primary flywheel 2 and the secondary flywheel 3, each cam follower 11 cooperates with only one arcuate portion of the blades 9, the other arcuate portion not being solicited. Typically, each cam follower 11 bends only one of the first and second blades during a relative rotation between the primary flywheel and the secondary flywheel 3. In other words, over the entire range of operation of the dual damping flywheel, that is to say, whatever the torque transmitted between the primary flywheel 2 and the secondary flywheel 3, each cam follower 11 cooperates with one or other of the blades 9a, 9b.
    [0017] Such a configuration of the damping means makes it possible to reduce the stress of the blades during use. More particularly, this configuration of the damping means prevents a same portion of the blade 9 is constrained both during a transmission of torque between the primary flywheel 2 and the secondary flywheel 3 in the retro direction 21 that in the direct direction 24. The portion of the blade 9 biased 25 during a transmission of torque between the primary flywheel 2 and the secondary flywheel 3 in the retro direction 21 is "independent" of the portion of the blade 9 requested when a transmission of torque between the primary flywheel 2 and the secondary flywheel 3 in the forward direction 24. This independence of the portions of the blade 9 biased according to the direction of torque transmission between the primary flywheel 2 and the flywheel 3 also allows 3 to achieve independent cam surfaces. That is, the cam surfaces being carried by distinct arcuate portions, they may have distinct stiffness and radius of curvature characteristics such that the cooperation between the cam surface the blade 9 and the corresponding cam follower is not related to the cooperation between the cam surface of the other portion of the blade 9 and the corresponding cam follower. In addition, the axial superposition of the blades 9 makes it possible to lengthen the circumferential length of the blades 9 and thus to obtain a better damping of the vibrations and acyclisms with a large angular displacement. The damping flywheel 1 can also be equipped with a friction assembly arranged to exert a friction-resistant torque during the relative rotation between the primary and secondary flywheels 3. The friction assembly is thus able to dissipate by friction. accumulated energy in the blades 9. FIG. 4 is a front view of a double damping flywheel of FIG. 1 having a relative rotation between the primary flywheel and the secondary flywheel and in which the secondary flywheel is not shown in order to to visualize the blades. In a relative rotation between the primary flywheel 2 and the secondary flywheel 15 in the forward direction 24, the first cam follower 1a moves from the angular position of rest along the cam surface 18 of the first portion. arcuate 14 of the first blade 9a. The second blade 9b is shown in dashed lines in areas where the first blade 9a and the second blade 9b are axially superimposed. The radius of curvature of the first arcuate portion 25 of the second blade 9b is such that the first cam follower 11a does not cooperate with said first arcuate portion 25 of the second blade 9b. Similarly, the second cam follower 11b cooperates with the second arcuate portion 26 of the second blade 9b only. Thus, the return force reminding the primary flywheel 2 and the secondary flywheel 3 towards their rest position results from the flexing of the first arcuate portion 14 of the first blade 9a and the flexion of the second arcuate portion 26 of the second 9b blade that are the only portions urged during a relative rotation between the primary flywheel 2 and the secondary flywheel 3 in the forward direction 24. In order to reduce parasitic friction may affect the damping function, the roller 20 is advantageously mounted in rotation on the primary flywheel 2 by means of rolling members (not shown), such as balls, rollers or needles. The roller 20 is for example carried by a cylindrical rod 29 extending parallel to the axis of rotation X and one end of which is fixed inside a bore (not shown) formed in the primary flywheel 2. Moreover, , the cylindrical rod 29 is received inside a through orifice 5 formed in a sleeve 30. The roller 20 is rotatably mounted around the sleeve 30. To do this, the rolling elements cooperate, on the one hand , with a rolling track formed on the outer periphery of the sleeve 30 and, on the other hand, with a raceway formed on the inner periphery of the roller 20.
    [0018] Figures 5 and 6 are front views of a dual damping flywheel of Figure 1 having a maximum relative rotation between the primary flywheel 2 and the secondary flywheel 3 respectively in the forward direction 24 and in the retro direction 21. In these figures 5 and 6, the secondary flywheel is not shown to view the blades 9.
    [0019] The double damping flywheel 1 advantageously has an abutment capable of limiting the relative deflection between the primary flywheel 2 and the secondary flywheel. This abutment comprises, for example, two projections 31 fixed on the secondary flywheel which each cooperate with a respective abutment surface 32 when they come into abutment, said abutment surfaces 32 being fixed on the primary flywheel 2. The abutment surfaces 32 are for example formed around each cam follower 11 as illustrated in FIGS. 5 and 6. FIG. 7 is a view front of a double damping flywheel according to another embodiment in which the secondary flywheel is not shown to view the blades. With reference to FIGS. 7 to 9, the elements of the double damping flywheel 25 having a shape and / or a function similar to the corresponding elements illustrated with reference to FIGS. 1 to 6 bear the same references increased by 100. In this second embodiment, the damping means has an asymmetry.
    [0020] In the illustrated embodiment, in order to obtain an asymmetric damping means, each blade 109a is asymmetrical. That is, the first arcuate portion 114 of the first blade 109a and the second arcuate portion 116 of the first blade 109a are not symmetrical. Here it will be noted that the second arcuate portion 116 on which the second support member rests is shorter than the first arcuate portion 114 on which the first support member rests. The first blade 109a and the second blade 109b projected in a plane perpendicular to the axis of rotation X remain however symmetrical with respect to the axis of rotation X. A second variant, not shown, provides on the contrary that the first arcuate portion 114 the second arcuate portion 116 of the first blade 109a is symmetrical but the first blade 109a and the second blade 109b projected in a plane perpendicular to the axis of rotation X are not symmetrical with respect to the axis of rotation X In each of these variants, the asymmetry of the damping means causes a difference in circumferential length of the cam surfaces of the blades 109 between the forward direction 124 and the backward direction 121. Thus, in the rest position as illustrated in Figure 7, the cam surface 118 of the first arcuate portion 114 of the first blade 109a has a circumferential length greater than the circumferential length of the cam surface 123 of the second arcuate portion 116 of said first blade 109a. Likewise, the cam surface 127 of the second arcuate portion 126 of the second blade 109b has a circumferential length greater than the circumferential length of the cam surface 128 of the first arcuate portion 125 of the second blade 109b. The asymmetry of the damping means thus makes it possible to obtain stiffness characteristics and / or maximum deflection angles that are different depending on whether a driving torque is transmitted (forward direction) or whether a resisting torque is transmitted. (Retro direction) .. Figures 8 and 9 show a front view of a double damping flywheel 101 of Figure 7 in a position of maximum relative rotation respectively in retro and forward direction. In these figures 8 and 9, the secondary flywheel 103 is not shown in order to display the blades 109. As illustrated in FIGS. 8 and 9, the double damping flywheel according to the second embodiment, the angular displacement between the flywheel The other characteristics of the blades and the cam followers, however, remain the same as those of the first embodiment, the primary 102 and 3033857 20 the secondary flywheel 103 is greater in the forward direction 124 relative to the retro 121 direction. For example, each blade 109 is secured with two rivets 104 or, in the rest position, the cam followers 111 are simultaneously in contact with the corresponding cam surfaces of the two blades 109. has been described in connection with several particular embodiments, it is obvious that it is not limited thereto and that it includes all the technical equivalents of the means described and their combinations if they fall within the scope of the invention. In particular, in an alternative embodiment not shown, the structure is reversed and the blades are fixed on the primary flywheel 2 while the rollers are carried by the secondary flywheel 3. The use of the verb "to include", "to understand" or "include" and its conjugate forms does not exclude the presence of other elements or steps other than those set forth in a claim. The use of the indefinite article "a" or "an" for an element or a step does not exclude, unless otherwise stated, the presence of a plurality of such elements or steps. In the claims, any reference sign in parentheses can not be interpreted as a limitation of the claim.
    权利要求:
    Claims (16)
    [0001]
    REVENDICATIONS1. Torsional damper for a torque transmission device comprising: - a first element (3, 103) and a second element (2, 102) movable in rotation relative to one another about an axis of rotation X, and - a blade damping means (9, 109) capable of transmitting a rotational torque between the first element and the second element and damping the rotation acyclisms between the first element (3, 103) and the second element ( 2, 102); the blade damping means comprising: a first resiliently deformable blade (9a, 109a) and a second resiliently deformable blade (9b, 109b), the first blade (9a, 109a) and the second blade (9b, 109b) being integral in rotation of the first element (3, 103), and o a first support member (11a, 111a) carried by the second element (2, 102), in which the first support member (11a, 111a), the first blade (9a, 109a) and the second blade (9b, 109b) are arranged such that: - the first support member (11a, 111a) cooperates with the first blade (9a, 109a) by bending it for transmitting a torque from the second element to the first element, and - the first support member (11a, 111a) cooperates with the second blade (9b, 109b) by bending it to transmit a torque from the first element to the second element .
    [0002]
    A torsion damper according to claim 1, wherein the first support member (11a, 111a), the first blade (9a, 109a) and the second blade (9b, 109b) are arranged such that the first member (11a, 111a) cooperates only with the first blade (9a, 109a) when a torque is transmitted from the second member to the first member and only with the second blade (9b, 109b) when a torque is transmitted from the first element to the second element. 3033857 22
    [0003]
    A torsion damper according to claim 1 or 2, wherein the first support member (11a, 111a), the first blade (9a, 109a) and the second blade (9b, 109b) are arranged such that at least a portion of the torque is transmitted by the first blade regardless of the value of a torque transmitted from the second element to the first element and at least a portion of the torque is transmitted by the second blade regardless of the value a torque transmitted from the first element to the second element.
    [0004]
    4. torsion damper according to any one of claims 1 to 3, wherein, for the entire range of operation of the damper, the first support member (11a, 111a), cooperates with at least one first and second blades. 15
    [0005]
    A torsion damper as claimed in any one of claims 1 to 4, wherein the blade damping means is arranged such that for a transmission of a torque from the second member to the first member a relative rotation in a first direction of rotation (21, 121) between the first and second members (2, 102, 3, 103) from an angular rest position occurs and the blade damping means exerts a first restoring force for recalling the first and second elements (2, 102, 3, 103) to their angular rest position, and for a transmission of a torque from the first element to the second element, a relative rotation in a second direction of rotation (24). , 124) opposite to the first direction of rotation between the first and second members (2, 102, 3, 103) from the angular rest position is made and the blade damping means exerts a second restoring force to recall the first and second elements (2, 102, 3, 103) to their angular rest position; the first bearing member (11a, 111a), the first blade (9a, 109a) and the second blade (9b, 109b) being arranged such that for relative rotation in the first direction of rotation (21, 121) between the first and second elements (2, 102, 3, 103) from the angular position of rest, the first support member (11a, 111a) cooperates with the first blade (9a, 109a) and exerts a force of bending on said first blade (9a, 109a), the bending of the first blade (9a, 109a) producing on the first bearing member (11a, 111a) the first restoring force, 3033857 23 - for a relative rotation according to the second direction of rotation (24, 124) opposite the first direction of rotation (21, 121) between the first and second members (2, 102, 3, 103) from the angular position of rest, the first support member (11a 111a) exerts a bending force on the second blade (9b, 109b), the bending of the second blade (9b, 109b) producing on the first bearing member (11a, 111a) l a second recall force.
    [0006]
    The torsion damper according to claim 5, wherein the first support member (11a, 111a) is simultaneously in contact with the first blade (9a, 109a) and with the second blade (9b, 109b) in the position angular rest.
    [0007]
    A torsion damper according to any one of claims 1 to 6, wherein each blade (9, 9a, 9b, 109, 109a, 109b) comprises: a first resiliently deformable section (14, 114, 25, 125 ), a second elastically deformable section (16, 116, 26, 126), - a fixing section (15) fixed relative to the first element (3, 103), and wherein the damper further comprises a second member bearing (11b, 111b) carried by the second member (2, 102), the first bearing member (11a, 111a), the second bearing member (11b, 111b), the first blade (9a , 109a) and the second blade (9b, 109b) being arranged such that: - the first support member (11a, 111a) cooperates with the first deformable section (14, 114) of the first blade (9a, 109a). ) by bending it and the second bearing member (11b, 111b) cooperates with the second deformable section (26, 126) of the second blade (9b, 109b) by bending it to transmit a torque of the second element to the first element, and - the second support member (11b, 111b) cooperates with the second deformable section (16, 116) of the first blade (9a, 109a) by bending it and the first member (11a , 111a) cooperates with the first deformable section (26, 126) of the second blade (9b, 109b) by flexing it to transmit a torque from the first member to the second member. 3033857 24
    [0008]
    Torsion damper according to claim 7, wherein the securing section (15) of each blade (9, 109) is located between the first deformable section (14, 114, 25, 125) and the second deformable section (16). 116, 26, 126) of said blade (9, 109). 5
    [0009]
    A torsion damper according to claim 7 or 8, wherein each blade has an axis of symmetry, a projection of the first blade in a plane perpendicular to the axis of rotation X being symmetrical to a projection of the second blade in said plane perpendicular to the axis of rotation X with respect to the axis of rotation X.
    [0010]
    A torsion damper according to one of claims 7 to 9, wherein each blade is asymmetrical, a projection of the first blade in a plane perpendicular to the axis of rotation X being symmetrical to a projection of the second blade in said plane perpendicular to the axis of rotation X with respect to the axis of rotation X.
    [0011]
    The torsion damper according to one of claims 1 to 10, wherein the first and second blades (9a, 109a, 9b, 109b) are attached independently of one another to the first member ( 3, 103).
    [0012]
    The torsion damper according to one of claims 1 to 11, wherein the first blade and the second blade are axially stacked (9a, 109a, 9b, 109b).
    [0013]
    13. torsion damper according to one of claims 1 to 12, wherein the first blade (9a, 109a) is fixed on the first member (3, 103) in axial abutment against said first element (3, 103), torsion damper further comprising a spacer (10), the second blade (9b, 109b) being fixed on the first member (3, 103) in axial abutment with the spacer (10), the spacer (10) being axially interposed between the second blade (9b, 109b) and the first element (3, 103), a portion of the first blade (9a, 109a) and a portion of the second blade (9b, 109b) being axially superimposed. 3033857 25
    [0014]
    A torsion damper according to any one of claims 1 to 13, further comprising an end stop (31, 32) so as to limit the relative rotation between the first member (3, 103) and the second member (2, 102,). 5
    [0015]
    15. torsion damper according to one of claims 1 to 14, wherein each blade (9, 109) is fixed on the first element by two rivets (4, 104). 10
    [0016]
    A torsion damper according to any one of claims 1 to 15, wherein each first and second blades has a cam surface and the first support member comprises a cam follower arranged to cooperate with the cam surface of the cam. first blade (9a, 109a) for transmitting a torque from the second member to the first member and with the cam surface of the second blade (9b, 109b) for transmitting a torque from the first member to the second member.
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    同族专利:
    公开号 | 公开日
    WO2016146415A1|2016-09-22|
    FR3033857B1|2017-10-20|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US6176785B1|1998-05-08|2001-01-23|Ellergon Antriebstechnik Gmbh|Torsional vibration damper or torsionally elastic and vibration damping coupling|
    FR2838490A1|2002-04-10|2003-10-17|Valeo|Automobile double damping flywheel comprises two coaxial flywheels connected by radial strips elastically deformable in bending, strips encastered at external radial end in intermediate ring free to rotate relative to flywheels|
    DE102012015014A1|2012-07-28|2014-01-30|GM Global Technology Operations LLC |Dual mass flywheel for vehicle drive train of motor vehicle, has primary rotational flywheel mass coupled with drive shaft of vehicle drive train, where secondary rotational flywheel mass is coupled to output shaft of vehicle drive train|
    FR3002605A1|2013-02-22|2014-08-29|Valeo Embrayages|TORSION DAMPER FOR CLUTCH FRICTION DISC|FR3061252A1|2016-12-23|2018-06-29|Valeo Embrayages|TORSION DAMPER WITH BLADES|FR3000155B1|2012-12-21|2015-09-25|Valeo Embrayages|TORSION DAMPER FOR A TORQUE TRANSMISSION DEVICE OF A MOTOR VEHICLE|US10288144B2|2016-02-11|2019-05-14|Valeo Embrayages|Transmission torque converter device|
    FR3057323A1|2016-10-06|2018-04-13|Valeo Embrayages|TORSION DAMPER WITH BLADES|
    FR3069601B1|2017-07-28|2019-08-23|Valeo Embrayages|LIMIT SWITCH DEVICE FOR A TORSION DAMPER|
    法律状态:
    2016-03-31| PLFP| Fee payment|Year of fee payment: 2 |
    2016-09-23| PLSC| Search report ready|Effective date: 20160923 |
    2017-03-31| PLFP| Fee payment|Year of fee payment: 3 |
    2018-03-29| PLFP| Fee payment|Year of fee payment: 4 |
    2019-11-29| ST| Notification of lapse|Effective date: 20191106 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1552113A|FR3033857B1|2015-03-16|2015-03-16|TORSION DAMPER|FR1552113A| FR3033857B1|2015-03-16|2015-03-16|TORSION DAMPER|
    PCT/EP2016/054751| WO2016146415A1|2015-03-16|2016-03-07|Torsional damper|
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