DE3520853C2 - Device for compensating torsional shocks - Google Patents

Description

The invention relates to a Device for compensating for rotary shocks, in particular re of torque fluctuations of an internal combustion engine, by means of at least two, arranged coaxially to one another neter, against the action of a damping device rotatable relative to each other and via a roller bearing stored and centered centrifugal masses, of which the one - first - with the internal combustion engine and the other - second - with the input part of a gearbox ver is binding, the damping device at least from in Effective energy stores exist circumferentially.

Facilities of this type are, for example, in the older application DE-OS 34 11 239 and in DE-PS 29 31 423 - shown here with a plain bearing.

The object of the present invention was to provide such a device improvements to improve, especially with regard to the construction or Structure, wear resistance and function, continue to be possible Liche application of such facilities to enlarge. In addition, should ensures cost-effective production of such devices his.  

According to the invention, this is achieved in a device of the type described be that
In addition to this damping device, at least one further damping device, which also contains at least circumferentially effective energy storage, is provided in the torque transmission path between the flywheels, the two damping devices are provided in series connection with one another, both the first damping device and the further damping device each having at least two , Have axially spaced disks and each disk group is articulated to a different one of the flywheels and that a one-piece, between two pairs of the different from the flywheels disks effective, common flange for torque transmission between the first and further damping device is seen before and at least one disc of the disc group connected to the first flywheel mass can be axially displaced to the first flywheel mass.

It can be an advantage if the disc against the effect of a Energy storage is relocatable.

Furthermore, it can be advantageous if the Inertia masses are rotatable to each other.  

It can be appropriate if the Intermediate flange radially covers both pairs of disks, whereby, in order to Axial direction to ensure particularly short overall length, it especially can be useful if the one group of disks at least essentially Lichen is provided radially within the other and the flange both Disc groups radially covered.

A particularly advantageous embodiment of the device can be given be when the input part of the further damping device by the disc group connected to the first flywheel is formed, the Output part through the intermediate flange, which is also the input part of the forms the first damping device, the output part by the two is connected to the second flywheels connected discs. It can be particularly advantageous if for possible rotation both flywheels to each other between the intermediate flange and the radially inner disc group and / or the intermediate flange and the radial outer group of disks a positive connection can be established. Such a positive connection can be formed by forming a stop contours on the flange and on or on the disc groups, which interact with each other.  

According to a further embodiment of the invention, it can be appropriate if the pair of washers of the first damping device with the second Flywheel, which can be connected to the input part of a transmission, is rotationally fixed and the pair of discs of the further damping device with the first one, which is connected to the internal combustion engine. Advantage However, it can also be if the pair of disks is the first Damping device with the first flywheel is rotatable and that Pair of discs of the other damping device with the second Flywheel.

A particularly simple construction of the further damping device can be ensured if the intermediate flange is axially between the pair of discs of the further damping device for generating a Slip torque is clamped. It may vary depending on the size of the required Lichen slip torque be advantageous if the flange and the two Rub the discs of the other damping device directly against each other. For the vast majority of applications, however, it will be appropriate at least between one of the disks of the further damping device and to provide the flange with a friction or sliding lining, so that by ent speaking friction or sliding pads the slip moment at the respective Application can be adapted.

The axial bracing of the flange between the pair of washers can further damping device in a particularly simple manner ensure that a disc of the further damping device axially fixed to one of the flywheels and the other disc against over this is axially displaceable. The axial can expediently secure the other disc against rotation. This twisting  fuse between the two discs of the further damping device can advantageously take place in that at least one of the disks has axial projections which cut into the other disc to grab. This can result in a particularly simple structure, if these projections are integrally attached to at least one of the disks shaped, axially extending tabs are formed, which in The outer circumference of the other disk provided cut-outs axially Depending on the application, it may be appropriate if this before jumps the axially fixed disc and / or the axially displaceable Disc of the further damping device carries. Furthermore, it can be from Be an advantage if the axial projections on the radially outer circumference are at least at least one of the disks of the further damping device is provided are so that they can axially overlap the intermediate flange on the outside. The axial fixation of at least one of the washers of the other dampers tion device on one of the flywheels can according to another Feature of the invention done by a rivet connection.

To generate a slip moment between the pair of disks additional damping device and the intermediate flange, it can be special be advantageous if the axially displaceable disc of the further dampers tion device by an energy store axially in the direction of the other Disc is applied. By appropriate interpretation of the The energy accumulator can thus reduce the slip moment of the further damping equipment varies and adapted to the respective application will. It can be appropriate if the axially left The energy accumulator acting on the disc is swinging supported on which the axially fixed disc is also attached is.  

In an advantageous manner, the energy accumulator can be provided by a tellerfe be formed such an element, this ge on the circumference slits or can be open and the outer periphery of the same a shoulder of the flywheel on which the plate spring-like Element is supported. Such slit on the circumference or open, plate spring-like elements can be particularly easy to produce by rolling a strip of material. Furthermore, such a plate spring-like element can be simplified Way in which it is mounted comprehensive groove or shoulder.

According to a further feature of the invention, the at least at least one of the discs of the further damping device Anti-rotation provided axial projections by free protruding cuts in the flange. These cuts can be made in advantageously introduced on the outer circumference of the flange and if necessary, be open to the outside. Can be particularly useful be there when between the clearances and the protrusions in the circumferential direction at least in the possible angle of rotation corresponding damping device corresponding game is available. Furthermore, it may be appropriate if at least some of the axial projections to limit the angle of rotation of the others Damping device on the contours of the free cuts of the flan come to the plant. These stop contours for the projections at least one of the disks of the further damping device can advantageously be formed by radial arms be formed by the flange on its outer periphery. Thus, the angle of rotation of the further damping device  by the flange of the flange resting on axial projections at least one of the disks of the further damping device be limited.

According to a development of the invention, it can be useful if in the pair of discs of the further damping device in Recesses aligned in the axial direction to accommodate between these disks and the flange compressible energy stores are provided. It may be appropriate if this force store in the end regions of the angle of rotation of the others Damping device take effect.

Such energy stores can advantageously as Impact body to limit the angle of rotation of the other dampers serving device. This avoids, for example between the arms of the flange and the two washers of the further damping device in the end regions of the twisting winch kels this further damping device a hard impact arises, and noise can thus be avoided. Purpose It can be moderate if the lift mechanism is operated by coil springs and / or rubber blocks are formed. It can be useful if the lift mechanism, in the circumferential direction between the arms seen of the flange, can be acted upon directly by this are.

According to an additional feature of the invention, it can be special be inexpensive if the between the flange and at least one of the discs of the further damping device effective Friction lining by individual, on the arms of the flange Stigt segments is formed from friction or sliding material.  

Furthermore, it can be advantageous if the flange by at at least one of the flywheels is guided concentrically.

A particularly advantageous embodiment of the device can be given if at least one of the flywheels has a ringar term, extend axially in the direction of the other flywheel has the extension, radially within which the further damper tion device and the first damping device arranged are. It can be useful if the extension is the further Damping device overlaps axially, because then for some users cases advantageously the plate spring-like element, which is the axially displaceable disc of the further damping direction in an open end of the fort provided groove can be axially and radially supported. For other applications, however, it may also be appropriate if on the front side of the further damping device axially overlapping extension the axially fixed disc of the white tere damping device is attached so that between the Continuous flywheel and this disc a ringför miger space can be formed in which the flange radially into it protrude and in which the axially displaceable disc of the other Damping device can be added. It can be useful be there when the first, with the crankshaft of an internal combustion engine Machine-connected flywheel has the extension. In which the structure described last may still be appropriate if the plate spring-like element of the further damping device tion between the first flywheel and the axially displaceable Disc of the further damping device is clamped.  

According to a development of the invention, concentric Guide of the flange molded on the outer circumference of the flange Boom radially on the axial extension of the flywheel support. With such a structure it can be avoided that the function of the first damping device due to external friction is affected. This is especially for those twisting areas of the first damping device in which the between the moment transferred to the two flywheels is relatively small is particularly advantageous. It may still be useful if between the extension of the corresponding flywheel and the A friction or sliding lining is provided for the flange, which is used for the radial guidance of the flange. On The structure of the device can be particularly advantageous. if at least individual arms of the flange are each one cap made of friction and / or sliding material is encompassed, which on the one hand ensures the radial guidance of the flange and on the other hand to generate a frictional torque between the sheaves ben the other damping device and the flange clamped is. The caps can advantageously - in scope viewed in the direction - elastically deformable at its end areas Molded stop areas that limit with stops tion of the angle of rotation of the further damping device together can work.

According to an additional feature of the invention Centering the flange at least some of its arms - in Considered circumferential direction - from one on the axial extension the corresponding flywheel supporting bow-like guide  around shoes are encompassed, the advantageously Side legs of the bracket-like guide shoes or guide bracket with stops to limit the backlash of the others Damping device can interact. These attacks can for example, axially between the two disks extending connecting means, or, as already described ben, by in the recesses of the two discs of the other dampers tion device recorded energy storage, or by stops provided on the extension of the corresponding flywheel be educated. Furthermore, it can be advantageous if between the side legs of the guide bracket and the arms of the flan There is circumferential play. It can be attached also be if between the side legs of the guide bracket and an energy accumulator is provided for the arms of the flange.

Such energy stores can advantageously by a elastic material, such as rubber, be formed. This power spit Avoid a too hard stop in the end areas of the further damping device, whereby noises are avoided can.

To limit the possible between the two masses Angle of rotation, it can also be advantageous if between Flange and the second flywheel stops to limit the Angular deflection of the first damping device are provided. It can be appropriate if the stops by distance bolts are formed, on the one hand the washers of the first Damping device with each other and on the other hand with the two Connect the flywheel and cut through the flange  protrude axially. It can be useful if by Stop the spacer bolts at the end areas of the cutouts in the Flange limited the angle of rotation of the first damping device becomes. Advantageously, the cutouts in the Flange be arranged and designed such that the flange on its inner periphery has radial teeth that between the Grab the spacer. It can be advantageous if the Teeth through the introduction of cutouts in the radially inner Areas of the flange are formed. By attacking the connecting two disks of the first damping device Spacers on the teeth of the flange can thus twist hung the flange against the corresponding flywheel be limited.

According to a further embodiment of the invention can the discs of the other damping device via Ab steady, such as spacers to be axially fixed to each other and at least one of the washers between the spacer bolts in the circumferential direction resiliently biased corrugation point, which clamps the flange towards the other disc. With such a construction of the further damping device a special energy accumulator for bracing the two discs the further damping device towards each other is not required Lich. With such a structure, it is also advantageous if the damping between the two washers direction provided spacer bolts for fastening at the same time serve the discs on one of the flywheels.  

Furthermore, it can be advantageous if the further damping is direction is designed such that the two sides of the flange provided washers by means of spring bars distributed over the circumference gel or clamps can be clamped against the flange. Appropriate it can be when the bracket or brackets the flange and axially over the two disks of the further damping device grasp and with radial legs the discs axially reach behind and apply in the direction of the flange. The Legs of the bracket or brackets can be advantageous extend way radially inwards.

Furthermore, it can be advantageous if one of the flywheels has axial projections in cutouts of the flange flanking flanks of the other damping device fen, for their rotation lock. It can be particularly advantageous if - viewed in the circumferential direction - between the axial Projections formed on the circumference of the flange radially engage and energy storage in recesses of the discs further damping device are included, which as Endan beat to limit the angle of rotation of the further damping device for the arms of the flange. Furthermore can it should be useful if at least individual recesses for Inclusion of the energy storage of one disc compared to them axially opposite recesses of the other disc in The circumferential direction are offset such that the axially opposite recesses recorded the energy store Discs against which cutouts of the discs penetrate brace the projections in the circumferential direction. This will  Avoided noises. It may be appropriate if the axial Projections are formed by bolts or pins on one the flywheels are attached.

According to a further embodiment of the invention, it can be advantageous be when the flange in the area between the discs of the white tere damping device has axial recesses in which Friction blocks or friction linings are included, which between the Discs of the further damping device are clamped. For In some cases, it may be appropriate if the Recesses in the flange are axially continuous and through them one friction block each with a greater thickness than that of the flan extend through it. It can be advantageous if the friction blocks are axially displaceable in their recesses, in the radial and / or circumferential direction.

However, for some applications it can also be useful if the axial recesses arranged a pair of one behind the other Neten friction blocks between which an energy accumulator, such as For example, a plate spring is provided, the friction blocks clamped against the discs of the further damping device. Around it can enable simple installation of the device be advantageous if the pair of friction blocks and the Intermediate energy accumulator axially together via connecting means are kept, but the connecting means be a limited axial displacement of the two friction blocks to each other, against the effect of the energy store provided in between enable.  

When using friction blocks in the further damping device tion, it can be particularly advantageous if the flange is on has other blind holes to accommodate Friction blocks, the axially between each two directional blind holes existing partition of the Flange shows a breakthrough through which one, the pair of axially opposed friction blocks Connection means protrudes, between at least one the friction blocks and the intermediate wall an energy accumulator, like one Disc spring, which is arranged between the friction blocks Discs of the further damping device clamped and still the connecting means has a limited axial displacement of itself opposite blocks against the effect of the energy accumulator enable.

According to a further embodiment of the invention, it can in particular be advantageous if the first damping device is radial is provided within the further damping device.

The invention will be explained in more detail with reference to FIGS. 1 to 11.

It shows:

Fig. 1 a device according to the dung OF INVENTION shown in section,

Fig. 2 is a partial view according to arrow II, of the device shown in Fig. 1,

Fig. 3 shows a possible embodiment illustrated in the sectional view of another damping device for an inventive device,

FIGS. 4 and 5, another possible embodiment of a further damping means for an inventive device, Fig. 5 shows a section according to the line VV of Fig. 4,

Fig. 6 shows another possible embodiment of tung possibility of a further damping means for an inventive Einrich

FIGS. 7 and 8 and 9 and 10 further construction possible speeds of further damping means for a erfindungsge Permitted device, in which Fig. 8 shows a slice of the plate pair of the further damping means in the non-assembled state Fig. 9 shows a section according to line IX-IX of FIG. 10 represents

Fig. 11 is an additional possible embodiment of a further damping means for an inventive device.

The device 1 shown in FIGS . 1 and 2 for compensating rotary shocks has a flywheel 2 which is divided into two flywheels 3 and 4 . The first flywheel 3 is attached to a crankshaft 5 of an internal combustion engine, not shown, via fastening screws 6 . A friction clutch 7 is fastened on the second flywheel 4 by means not shown in detail. Between the pressure plate 8 of the friction clutch 7 and the flywheel 4 , a clutch disc 9 is provided, which is received on the input shaft 10 of a transmission, not shown. The pressure plate 8 of the friction clutch 7 is acted upon in the direction of the flywheel 4 by a plate spring 12 pivotably mounted on the clutch cover 11 . By actuating the friction clutch 7 , the flywheel 4 and thus also the flywheel 2 of the transmission input shaft 10 can be engaged and disengaged. Between the flywheel mass 3 and the flywheel mass 4 , a first damping device 13 and a further damping device 14 connected in series therewith are provided, which allow a limited relative rotation between the two flywheel masses 3 and 4 .

The two flywheels 3 and 4 are rotatably supported relative to each other via a bearing 15 . The bearing 15 comprises a rolling bearing in the form of a double row angular contact ball bearing 16 with part inner ring 17th The outer bearing ring 16 a of the rolling bearing 16 is in a bore 18 of the flywheel 4 and the inner split bearing ring 17 of the rolling bearing 16 is arranged on a central cylindrical pin 19 of the flywheel 3 extending axially away from the crankshaft 5 .

The two partial rings 17 a, 17 b of the inner ring 17 are braced axially by an energy accumulator in the form of a plate spring 20 . To secure the part of ring 17 is b from the end face 19 a of the pin 19, a lock washer 21 by means of screws 21 a BEFE Stigt which extends radially outwardly beyond the pins 19 hinauser and where the partial ring 17 b is axially supported. Arranged between ring portion 17 a and a flywheel 3 Belleville spring acts on the ring portion 17a axially towards the part of the ring 17 b by mass with radially outer regions on the flywheel 3 is supported and having radially inner portions against the portion of ring 17 a acts. As a result of this structure, the rolling elements of the bearing 16 are clamped between the roller tracks assigned to them. In order to ensure that the bearing remains tensioned even when the friction clutch 7 is actuated, the plate spring 20 applies a force which is greater than the maximum force required to actuate the friction clutch 7 . It has proven to be advantageous to choose the force generated by the plate spring 20 at least approximately twice as high as the maximum force required to disengage the friction clutch 7 .

The flywheel 3 has an axially radially outward extension 22 which forms a chamber 23 in which the first damping device 13 and the further damping device 14 are essentially accommodated. The input part of the further damping device 14 is formed by a disk group, namely the two disks 24 , 25 which are provided at an axial distance from one another and which are non-rotatable with the flywheel 3 . The ringförmi ge disk 25 is fixed on the end face 22 a of the extension 22 by means of rivets 26 and axially limited with the areas 25 a reach the chamber 23rd The disc 24 received in the chamber 23 has axial projections which are formed by tabs 24 a integrally formed on the outer circumference. For rotation of the disk 24 against the disk 25, the flaps 24 a 27 engage the disc 25 in the recesses. The recesses 27 and the flap 24 a are designed such that there is an axial possibility of publishing the disk 24 relative to the disk 25 . Radial arms 28 of the flange 29 are clamped axially between the two disks 24 and 25 , in that an energy store in the form of a plate spring 30, which is provided axially between the disk 24 and the flywheel 3 , acts on the disk 24 in the direction of the disk. For this purpose, the plate spring 30 is supported with radially outer areas on the pressure plate 3 and with radially inner areas on the disk 24 . The plate spring 30 is open or slotted on its circumference, ie that its annular base body is separated at one point, and is supported with its radially outer periphery on an annular shoulder 31 of the flywheel 3 radially. Between the arms 28 of the flange 29 and the two disks 24 and 25 are each friction linings in the form of individual, on the bracket 28 glued to Belagsegmen th 32 are provided. In the area between the arms 28 of the flange 29 , recesses 33 , 34 are introduced into the disks 24 and 25 , which are axially aligned and accommodate energy accumulator 35 . In the example shown, these energy accumulators are formed by helical springs 35 , but it could also, for. B. hard rubber springs can be used. The energy accumulator 35 serve as end stops for the arm 28 of the flange 29 and thus limit the angle of rotation of the further damping device 14 . The damping effect of the energy accumulator 35 prevents an excessively hard stop in the end regions of the angle of rotation of the further damping device.

As can be seen in particular from Fig. 2, in which the further damping device is shown in an intermediate position, there is a game 36 and 36 a between the energy stores 35 and the arms 28 , which increases by the amount by which the energy stores 35 are compressed can define the possible angle of rotation between the disks 24 , 25 forming the input part and the flange 21 forming the output part of the further damping device 14 .

The flange 29 forming the output part of the further damping device 14 also represents the input part for the first damping device 13. The first damping device 13 has a further group of disks, namely the two disks 37 , 38 arranged on both sides of the flange 29 , which are spaced apart by bolts 39 in the axial direction Spacing are connected to one another in a rotationally fixed manner and are articulated on the flywheel 4 . The two disks 37 , 38 are encompassed radially on the outside by the annular disks 24 , 25 of the further damping device 14 . Furthermore, in the example shown, the disks 37 and 24 and 38 and 25 are arranged at least approximately in the same plane. In the disks 37 and 38 and in the radially within the boom 28 areas of the flange 29 recesses 37 a, 38 a and 29 a are introduced, in which energy storage in the form of screw benfedern 40 are added. The energy accumulator 40 counteracts a relative rotation between the flange 29 and the two discs 37 , 38 .

The first damping device 13 also has a Reibein device 13 a, which is effective over the entire possible angle of rotation between the two flywheels 3 and 4 .

The friction device 13 a is arranged axially between the disk 37 and the flywheel 3 and has a force accumulator 41 formed by a plate spring, which is held clamped between the disk 37 and a pressure ring 42 , as a result of which the friction ring arranged between the pressure ring 42 and the flywheel 3 43 is clamped. The force exerted on the disk 37 by the plate spring 41 is intercepted by the bearing 16 . The pressure ring 42 is provided with arms 42 a, which grip around the head of the rivet 39 , whereby the pressure ring is non-rotatable with the flywheel 4th

On its radially inner periphery, the flange 29 has inwardly open cutouts 44 through which the spacer bolts 39 project axially. These cutouts form radially inwardly facing teeth 45 , which - viewed in the circumferential direction - engage between the spacer bolts 39 and cooperate with them as stops for limiting the angular deflection of the first damping device 13 .

The recesses 37 a, 38 a of the two disks 37 , 38 and the recesses 29 a of the flange 29 and the helical springs ( 40 ) provided therein are arranged and dimensioned over the circumference of the first damping device 13 such that a multi-stage damping characteristic curve is produced.

For at least approximately concentric guidance of the flange 29 with respect to the axis of rotation 47 and thus also with respect to the flywheels 3 and 4 , the flange 29 is supported with its radial arms 28 on the inner lateral surface 22 b of the axial extension 22 of the flywheel 3 .

The device according to the present exemplary embodiment is designed such that, starting from a rest position shown in FIG. 2, when a moment change occurs, the first flywheel 3 together with the pair of disks 24 , 25 and the flange 29 relative to the second flywheel 4 and the pair of disks 37 , 38 is rotated, namely against the action of the springs 40 , with a progressive increase in the damping effect taking place due to the different sized window openings in the flange 29 and in the pair of disks 37 , 38 . This Relativverdre hung takes place until the torque generated by the bracing of these springs reaches the friction torque that can be transmitted by the further damping device 14 . As the relative movement continues in this direction, the further damping device then begins to slip, with no relative rotation of the flange 29 relative to the second flywheel mass until the springs 35 strike the flanks of the extension arm 28 . The arms 28 cause a further relative rotation of the flange together with the first flywheel mass 3 with respect to the second flywheel mass 4 , the springs being further compressed until the teeth 45 come into contact with the bolts 39 .

As can be seen in particular from FIG. 2, in the embodiment shown in the embodiment, the arms 28 are designed in such a way that they limit the maximum angle of rotation of the further damping device 14 on the springs 35 . By appropriate modification of the stop contours of the arm 28 , the tabs 24 a could also be used. In such an embodiment, the respective stop contours of the extension arm 28 relative to the energy stores 35 and the flaps 24 a - viewed in the circumferential direction - should be arranged such that the energy stores first absorb the torque surges and then together with the flaps 24 a the rotation between the two Limit washers 24 , 25 and flange 29 . Furthermore, it would be possible to omit the energy accumulator 35 and only use the tabs 24 a to limit the angle of rotation between the input part and the input part of the further damping device.

In the embodiment variant shown in FIG. 3, the disk 125 , which is connected to the first flywheel 103 in a rotationally fixed manner via a rivet connection 126 , has radially externally formed and axially extending tabs 125 a. The tabs 125 a extend in the direction of the second flywheel 104 and engage axially in sections 127 , which are provided on the outer circumference of the disk 124 . The cutouts 127 and the tabs 125 a are matched to one another in such a way that the disk 124 is fixed relative to the disk 125 in the circumferential direction, but has an adjustment possibility in the axial direction. Between the two disks 124 and 125 forming the input part of the further damping device 114 , a flange 129 , which forms the output part of the further damping device 114 , is clamped. Between the flange 129 and the disks 124 , 125 , a friction lining 132 is arranged. The flange 129 at the same time forms the input part for the first damping device 113 , the output part of which is in turn formed by two disks 137 , 138 which are connected to one another via spacer bolts 139 and to the flywheel 104 in a rotationally fixed manner. The further damping device 114 and the first damping device 113 are in turn arranged radially within an axial extension 122 of the flywheel 103 . In the radially inner lateral surface of the extension 122 , a groove 131 is made in the region of the free end, on which a plate spring 130 is supported in both the axial and radial directions. For better assembly, this plate spring 130 is slotted or open at its circumference. With its radially inner areas, the disk spring 130 strikes the disk 124 axially in the direction of the disk 125 , as a result of which the flange 129 is clamped ben ben axially between these two disks and, via the axial force and the coefficients of friction between the friction linings 132 and the flange, the transferable slip torque of the further damping device is defined.

In the embodiment variant shown in FIGS. 4 and 5 of a further damping device 214 , friction or sliding linings 248 are arranged between the radially inner lateral surface 222 b of the axial extension 122 of the flywheel 203 and the arms 228 of the flange 221 . The flange 229 is guided concentrically to the flywheel 203 via these friction or sliding linings 243 . The friction or sliding linings 248 form approximately the bottom of caps 249 in the illustrated embodiment, which are placed on the boom 228 and encompass them. The lateral areas 250 , 251 of the caps 249 are clamped axially between the arms 228 of the flange 229 and the disks 224 , 225 arranged on both sides of the flange of the further damping device 214 in order to generate a frictional torque. The axial clamping is ensured by a plate spring 232 which axially acts on the disc 225 and is axially supported on the flywheel 203 . To radially secure the caps 249 against the centrifugal force, the lateral areas 250 , 251 on their side facing the arms 228 arcuate beads 250 a, 251 a, which engage in correspondingly adapted, arcuate grooves 152 of the arm 228 . In order to enable the caps 249 to be pushed onto the cantilevers 228 on account of their inherent elasticity, the beads 250 a, 251 a, viewed in the circumferential direction, only extend over a partial region of the extent of the grooves 252 or cantilevers 228 . The areas 253 , 254 of the caps 249 considered in the circumferential direction form elastic or shock-absorbing contact areas which cooperate with one another to limit the angle of rotation of the further damping device 214 with stops 255 which are non-rotatable with the flywheel 203 . The stops 255 are formed by pins or bolts which are anchored in the Schwungmas se 203 and axially reach through the recesses 256 to secure the disks 224 , 225 .

In the embodiment variant shown in FIG. 6, bow-like guide shoes 349 are provided for centering the flange 329 with respect to the flywheel 303 on the arms 328 of the flange 329 . The guide bracket 349 encompass the extension arm 328 , the radially extending side legs of the guide bracket interacting with stops 355 for limiting the angle of rotation of the further damping device 314 , which are non-rotatable with the inertia mass 303 . As in the embodiment shown in FIGS. 4 and 5, the stops 355 are formed by pins or bolts which are anchored in the flywheel 303 and which axially extend through the flanges 329 arranged on both sides of the flange of the further damping device 314 . The area 349 a connecting the two legs 353 and 354 of the guide bracket 349 is guided between the radially inner lateral surface 322 b of the axial extension 322 of the flywheel 303 and the radially outer lateral surface of the arm 328 . , The guide bracket 349 - considered in circumferential direction - a greater extent than that of the arm 328, so that on both sides of the cantilever 328 between them and the side legs 353, 354 of the guide bracket 349, a clearance X is present. In the free spaces formed by the game X, energy storage in the form of hard rubber blocks 357 are easily seen. This hard rubber blocks 357 cause a damping of the impact between the side legs 353 , 354 and the stops 355 . The shoes 349 can be made of metal or friction or sliding material.

In Figs. 7 and 8, the two disks 424, 425 by means of spacing means in the form of standoffs 455, both miteinan of, and firmly connected to the flywheel mass 403rd Between the two disks 424, 425 engage radial arm 428 of a flange 429, wherein between the arms 428 and the two discs 424, 425 a friction lining is provided 432nd

As is apparent from Fig. 8, has the disc 425 between the mounting holes 455 a for the standoffs 455 a circumferential direction extending in the order corrugation 425 a, which is biased in the mounted state of the disc 425, as can be seen from Fig. 7. Due to this biasing of the flange 429 and the boom 428 axially between the discs 424, 425 is clamped, so that a corresponding friction torque occurs at a relative rotation. To limit the angle of rotation of the white damping device 414 in turn recesses 424 , 425 energy stores 435 are provided, on which the boom 428 of the flange 429 come to rest.

In the embodiment shown in FIGS. 9 to 11, the disks 524 , 525 provided on both sides of the flange 529 of the further damping device 514 are clamped against the flange 529 by means of spring clips or spring clips 530 distributed over the circumference with the interposition of a friction ring 532 . The brackets or clamps 530 overlap the flange 529 and the two disks 524 and 525 axially and act on the disks 524 , 525 with spring legs 530 a, 530 b directed radially inwards. To secure the discs 524 , 525 are provided on the flywheel 503 axial projections in the form of bolts 555 , which protrude axially through holes 555 a, 555 b of the discs 524 , 525 adapted to them.

In the disks 524 , 525 recesses 533 , 534 are provided for receiving energy accumulator 535 , which cooperate with the arms 528 of the flange 529 to limit the angle of rotation of the further damping device 514 .

As can be seen from FIG. 10, in the assembled state of the discs ben 524 and 525, the recesses 533 of the disc 524 are offset by an amount Y in the circumferential direction relative to the recesses 534 of the disc 525 , as a result of which the force accumulator 335 between the discs 524 , 525 on one side or respectively be axially clamped asymmetrically. This asymmetrical bracing of the energy accumulator 335 in turn causes the disks 524 , 525 to be braced in the circumferential direction against the bolts 555 projecting through the holes 555 a, 555 b. The function of the further damping device 514 is significantly improved due to this bracing, since a play z. B. between the holes 555 a, 555 b of the washers 524 , 525 and the bolts 555 can be compensated for, so that a damping effect is always present with a relative rotation.

In the embodiment of a further damping device 614 shown in FIG. 11, the flange 629 in the area between the disks 624 and 625 , which form the input part of the further damping device 614 , has axially directed blind holes 656 , 657 , in each of which a disc-shaped one Friction lining 658 , 659 is added. The remaining between the two blind holes 656 and 657 intermediate wall 660 of the flange 629 has an opening 661 through which a Ver connection means protrudes in the form of a rivet 662 , which axially connects the pair of axially opposite friction linings 658 , 659 . Axially between the friction lining 658 and the Zwischenwan extension 660 , a tensioned plate spring 663 is provided, which causes an axial expansion or an axial pressing apart of the two friction linings 658 and 659 , whereby these friction linings 658 , 659 against the corresponding disk 624 , 625 , with the they are in a friction connection, are pressed.

The connecting rivet 662 is dimensioned such that, starting from the installation position of the two friction linings 658 , 659 shown in FIG. 11, it enables a limited axial displacement of these friction linings 658 , 659 away from one another. This limited axial Verlager bility of the two friction linings 658, 659 enables the one hand a wear compensation of the friction pads 658, 659 and provides on the other hand ensures that when not yet mounted further Dämpfungsein device 614 the friction pads 658, 659 and the disc spring axially fixed on the flange 629,663 are, whereby the assembly of the device or the further damping device 614 is much easier. When installing the device or the white damping device 614 , the two friction linings 658 and 659 , against the action of the plate spring 663 , are axially clamped between the two disks 624 , 625 .

As can also be seen from FIG. 11, the friction lining 659 is supported axially directly on the intermediate wall 660 , whereas there is an axial free space between the friction lining 658 and the intermediate wall 660 , so that the friction block 658 , against the action of the plate spring 663 , can be shifted axially in the blind hole 656 .

Claims (72)

1.Device for compensating rotary shocks, in particular torque fluctuations of an internal combustion engine, by means of at least two coaxial mutually arranged, counter-rotating against the action of a damping device and centrifugal masses which are mounted and centered via a roller bearing, one of which - the first - with the internal combustion engine and the other - second - ver bindable to the input part of a transmission, the damping device consists at least in the circumferential direction of force accumulators and in addition to this damping device little least another, also at least circumferentially effective force accumulator containing damping device in the torque transmission path between the flywheels it is provided that the two damping devices are provided in series connection with one another, both the first damping device ( 13 , 113 ) and the further damping device ( 14 , 114 , 21 4 , 314 , 414 , 514 , 614 ) each have at least two disks arranged at an axial distance from one another ( 37 and 38 , 137 and 138 , 24 and 25 , 124 and 125 , 224 and 225 , 424 and 425 , 524 and 525 , 624 and 625 ) and each disc group is articulated to a different one of the centrifugal masses ( 3 , 4 , 103 , 104 , 203 , 303 , 403 , 503 ) and that a one-piece, between two pairs of those of the centrifugal masses ( 3 , 4 , 103 , 104 , 203 , 303 , 403 , 503 ) different washers ( 37 and 38 , 137 and 138 , 24 and 25 , 124 and 125 , 224 and 225 , 424 and 425 , 524 and 525 , 624 and 625 ) effective, common flange ( 29 , 129 , 229 , 329 , 429 , 529 , 629 ) for torque transmission between the first ( 13 , 113 ) and further damping device ( 14 , 114 , 214 , 314 , 414 , 514 , 614 ) is seen before and at least one Disc ( 24 , 124 , 224 , 225 , 524 , 525 , 624 ) of the disc group connected to the first flywheel mass ( 3 , 103 , 203 , 403 , 503 ) for the first swing Gmass is axially displaceable. 2. Device for compensating for rotary shocks according to claim 1, characterized in that the disc ( 24 , 124 , 224 , 225 , 524 , 525 , 624 ) can be displaced against the action of an energy accumulator ( 3 , 130 , 232 , 530 , 663 ) is. 3. Device for compensating rotary shocks according to one of claims 1 or 2, characterized in that the flywheels ( 3 , 4 , 103 , 104 , 203 , 303 , 403 , 503 ) can be rotated relative to each other. 4. Device for compensating rotary shocks according to one of claims 1 to 3, characterized in that the flange ( 29 , 129 , 229 , 329 , 429 , 529 , 629 ) radially both pairs of discs ( 37 and 38 , 137 and 138 ; 24 and 25 , 124 and 125 , 224 and 225 , 424 and 425 , 524 and 525 , 624 and 625 ) covered. 5. Device for compensating rotary shocks according to one of claims 1 to 4, characterized in that the one disc group ( 37 and 38 , 137 and 138 ) at least substantially radially within the other ( 24 and 25 , 124 and 125 , 224 and 225 , 424 and 425 , 524 and 525 , 624 and 625 ) is provided and the flange ( 29 , 129 , 229 , 329 , 429 , 529 , 629 ) both disc groups ( 37 and 38 , 137 and 138 ; 24 and 25 , 124 and 125 , 224 and 225 , 424 and 425 , 524 and 525 , 624 and 625 ) radially covered. 6. Device for compensating rotary shocks according to one of claims 1 to 5, characterized in that the input part of the further damping device ( 14 , 114 , 214 , 314 , 414 , 514 , 614 ) by the with the first flywheel ( 3 , 103 ) connected disc group ( 24 and 25 , 124 and 125 , 224 and 225 , 424 and 425 , 524 and 525 , 624 and 625 ) is formed, the output part by the flange ( 29 , 129 , 229 , 329 , 429 , 529 , 629 ) , which also forms the input part of the first damping device ( 13 , 113 ), the output part of which is formed by the two disks ( 37 , 38 ; 137 , 138 ) connected to the two flywheel masses. 7. Device for compensating rotary shocks according to one of claims 1 to 6, characterized in that between the flange ( 29 , 129 , 229 , 329 , 429 , 529 , 629 ) and the radially inner group of disks ( 37 and 38 ; 137 , 138 ) and / or the flange ( 29 , 129 , 229 , 329 , 429 , 529 , 629 ) and the radially outer disc group ( 24 and 25 , 124 and 125 , 224 and 225 , 424 and 425 , 524 and 525 , 624 and 625 ) a positive connection can be established. 8. Device according to one of claims 1 to 7, characterized in that the pair of discs ( 37 and 38 ; 137 and 138 ) of the first damping device ( 13 , 113 ) with the second flywheel ( 4 , 104 ) is rotationally fixed and that Pair of disks ( 24 , 25 ; 124 , 125 ; 224 , 225 ; 424 , 425 ; 524 , 525 ; 624 , 625 ) of the further damping device ( 14 , 114 , 214 , 314 , 414 , 514 , 614 ) with the first ( 3 , 103 , 203 , 303 , 403 , 503 ). 9. Device according to one of claims 1 to 5 or 7, characterized characterized in that the pair of discs of the first damper tion device with the first flywheel is rotatably and the pair of disks with the further damping device the second flywheel. 10. Device according to at least one of the preceding claims 1 to 9, characterized in that the flange ( 29 , 129 , 229 , 329 , 439 , 529 , 629 ) axially between the pair of disks ( 24 , 25 ; 124 , 125 ; 224 , 225 ; 424 , 425 ; 524 , 525 ; 624 , 625 ) of the further damping device ( 14 , 114 , 214 , 314 , 414 , 514 , 614 ) is clamped. 11. The device according to claim 10, characterized in that at least between one of the disks ( 24 , 25 ; 124 , 125 ; 224 , 225 ; 424 , 425 ; 524 , 525 ; 524 ; 624 , 625 ) of the further damping device ( 14 , 114 , 214 , 314 , 414 , 514 , 614 ) and the flange ( 29 , 129 , 229 , 329 , 429 , 529 , 629 ) a friction or sliding lining ( 32 , 132 , 249 , 432 , 532 , 658 , 659 ) is provided is. 12. Device according to one of claims 1 to 10, characterized in that a disc ( 25 , 125 ) of the further damping device ( 14 , 114 ) axially on one ( 3 , 103 ) of the Schwungmas sen ( 3 , 4 ; 103 , 104 ) is fixed and the other disk ( 24 , 124 ) is axially displaceable relative to this ( 25 , 125 ). 13. The device according to claim 12, characterized in that the axially fixed disc ( 25 , 125 ) secures the other ( 24 , 124 ) against rotation. 14. Device according to claim 12 or 13, characterized in that for securing against rotation at least one ( 24 , 125 ) of the disks ben ( 24 , 25 , 124 , 125 ) of the further damping device ( 14 , 114 ) axial projections ( 24 a; 125 a ) which engages in cuts ( 27 , 127 ) of the other disc ( 25 , 124 ). 15. Device according to claim 14, characterized in that the projections ( 24 a, 125 a) integrally formed on at least one of the disks ( 24 , 25 , 124 , 125 ), in the axial direction extending tabs ( 24 a, 125 a) are formed, which project axially into cutouts ( 27 , 127 ) provided on the outer circumference of the other disk. 16. The device according to claim 14 or 15, characterized in that the axially fixed disc ( 125 ) carries the projections ( 125 a). 17. The device according to claim 14 or 15, characterized in that the axially displaceable disc ( 25 ) carries the projections ( 25 a). 18. Device according to one of claims 14 to 17, characterized in that the axial projections ( 24 a, 125 a) on the radially outer circumference of at least one of the disks ( 24 , 25 , 124 , 125 ) of the further damping device ( 14 , 114 ) are provided. 19. Device according to at least one of claims 1 to 18, characterized in that the axial fixing of at least one ( 25 , 125 , 424 , 425 ) of the discs ( 24 , 25 , 124 , 125 , 424 , 425 ) of the further damping device on one ( 3 , 103 , 403 ) of the flywheels ( 3 , 4 , 103 , 104 , 403 ) by a rivet connection ( 26 , 126 , 455 ). 20. Device according to one of claims 11 to 19, characterized in that the axially displaceable disc ( 24 , 125 , 225 , 524 , 525 ) of the further damping device ( 14 , 114 , 214 , 514 ) by an energy accumulator ( 30 , 130 , 232 , 530 ) axially in the direction of the other disc ( 25 , 124 , 224 , 525 , 524 ). 21. The device according to claim 20, characterized in that the axially displaceable disc ( 24 , 124 ) acting force accumulator ( 30 , 130 ) is supported on the flywheel ( 3 , 103 ), on which also the axially fixed disc ( 25 , 125 ) is attached. 22. A device according to claim 21, characterized in that the force accumulator (30, 130) is formed by a cup-spring-like member (30, 130). 23. The device according to claim 22, characterized in that the plate spring-like element ( 30 , 130 ) at its periphery ge slits or is open and the outer periphery of this element from a shoulder ( 31 , 131 ) of the flywheel ( 3 , 103 ) who supports it, is included. 24. Device according to one of claims 14 to 23, characterized in that the axial projections ( 24 a, 125 a) protrude through free cuts in the flange ( 29 , 129 ). 25. The device according to claim 24, characterized in that between the free cuts and the projections ( 24 a, 125 a) in the circumferential direction there is at least one game corresponding to the possible angle of rotation of the further damping device ( 14 , 114 ). 26. The device according to claim 24 or 25, characterized in that at least some of the axial projections ( 24 a, 125 a) to limit the angle of rotation of the further damping device ( 14 ; 114 ) on the contours of the free cuts of the flange ( 29 , 129 ) come to the plant. 27. Device according to one of claims 1 to 26, characterized in that the flange ( 29 , 229 , 329 , 429 , 529 ) on its outer periphery has radial arms ( 28 , 228 , 328 , 428 , 528 ) which the Limit the angle of rotation of the further damping device ( 14 , 214 , 314 , 414 , 514 ). 28. The device according to claim 27, characterized in that the boom ( 28 ) for abutment on axial projections ( 24 a) at least one ( 24 ) of the discs ( 24 , 25 ) of the further damping device ( 14 ) come. 29. Device according to one of claims 1 to 28, characterized in that in the pair of discs ( 24 and 25 , 124 and 125 , 424 and 425 , 524 and 525 ) of the further damping device ( 14 , 114 , 214 , 414 , 514 ) axially aligned recesses ( 33 , 34 ; 533 , 534 ) for receiving between these disks and the flange ( 29 , 129 , 429 , 529 ) compressible force storage ( 35 , 435 , 535 ) are provided. 30. The device according to claim 29, characterized in that the energy accumulator ( 35 , 435 , 535 ) are effective in the end regions of the twist angle of the further damping device. 31. Device according to one of claims 29 or 30, characterized in that the energy accumulator ( 35 , 435 , 535 ) serve as an impactor to limit the angle of rotation of the further damping device. 32. Device according to one of claims 29 to 31, characterized in that the energy accumulator ( 35 , 435 , 535 ) are formed by coil springs. 33. Device according to one of claims 29 to 31, characterized characterized in that the energy accumulator through rubber blocks are formed. 34. Device according to one of claims 29 to 33, characterized in that the energy accumulator ( 35 , 435 , 535 ) in the circumferential direction between the arms ( 28 , 428 , 528 ) of the flange ( 29 , 429 , 529 ) is provided and actuated by this are beatable. 35. Device according to at least one of claims 1 to 34, characterized in that between the flange ( 29 ) and at least one of the disks ( 24 , 25 ) of the further damping device ( 14 ) effective friction lining by individual on the boom ( 28 ) the flange ( 29 ) attached segments ( 32 ) is formed from friction or sliding material. 36. Device according to one of claims 1 to 35, characterized in that the flange ( 29 , 229 , 329 ) by at least one ( 3 , 203 , 303 ) of the flywheels is guided concentrically. 37. Device according to one of claims 1 to 36, characterized in that at least one ( 3 , 103 , 203 , 303 , 503 ) of the centrifugal masses has a ring-like extension ( 22 , axially extending in the direction of the other centrifugal mass ( 4 , 104 ) 122 , 222 , 322 ), radially inside of which the further damping device ( 14 , 114 , 214 , 314 , 514 , 614 ) and the first damping device ( 13 , 113 ) are arranged. 38. Device according to claim 37, characterized in that the extension ( 22 , 122 , 222 , 322 ) overlaps the further damping device ( 14 , 114 , 214 , 314 , 514 , 614 ) axially. 39. Device according to at least one of the preceding Ansprü surface, characterized in that the diaphragm spring-like element ( 130 ), which acts on the axially displaceable disc ( 124 ) of the further damping device ( 114 ), is provided in an in the open end region of the extension ( 122 ) Groove ( 131 ) is axially and radially supported. 40. Device according to claim 37 or 38, characterized in that on the end face ( 22 a) of the extension ( 22 ), the axially fixed disc ( 25 ) of the further damping device ( 14 ) is fixed, so that between the extension ( 22 ) having flywheel mass ( 3 ) and this disc ( 25 ) an annular space ( 23 ) is formed, into which the flange ( 29 ) projects radially and in which the axially displaceable disc ( 24 ) of the further damping device ( 14 ) is received. 41. Device according to one of claims 37 to 40, characterized in that the first flywheel ( 3 , 103 , 203 , 303 , 503 ) has the extension ( 22 , 122 , 222 , 322 ). 42. Device according to at least one of the preceding Ansprü surface, characterized in that the diaphragm spring element ( 30 ) of the further damping device ( 14 ) between the first flywheel ( 3 ) and the axially displaceable disc ( 24 ) of the further damping device ( 14 ) clamped is. 43. Device according to at least one of the preceding Ansprü surface, characterized in that, for concentric guidance of the flange ( 29 , 229 , 329 ), the boom ( 28 , 228 , 328 ) of the flange on the axial extension ( 22 , 222 , 322 ) radially support one flywheel ( 3 , 203 , 303 ). 44. Device according to claim 43, characterized in that a friction or sliding lining ( 248 , 349 a) is provided radially between the extension ( 222 , 322 ) and the arms ( 28 , 228 ) of the flange ( 29 , 229 ). 45. Device according to claim 43 or 44, characterized in that at least individual arms ( 228 ) of the flange ( 229 ) are each encompassed by a cap made of friction and / or sliding material ( 249 ) which, on the one hand, guides the flange radially ( 229 ) and, on the other hand, is clamped between the disks ( 224 , 225 ) of the further damping device ( 214 ) to generate a frictional torque. 46. Device according to claim 45, characterized in that the caps ( 249 ) - viewed in the circumferential direction - have formed at their end regions elastically deformable stop areas ( 253 , 254 ) which with stops ( 255 ) to limit the angle of rotation of the further damping device ( 214 ) work together. 47. Device according to one of the preceding claims, characterized in that for centering the flange ( 329 ) at least some of its arms ( 328 ) - viewed in the circumferential direction - of a guide bracket ( 349 ) supported on the extension ( 322 ) of the inertia mass ( 303 ) ) are encompassed. 48. Device according to claim 47, characterized in that the side legs ( 353 , 354 ) of the guide bracket ( 349 ) interact with strikes ( 355 ) to limit the backlash of the further damping device ( 314 ). 49. Device according to claim 47 or 48, characterized in that there is play (X) in the circumferential direction between the side legs ( 353 , 354 ) of the guide bracket ( 349 ) and the cantilevers ( 328 ). 50. Device according to one of claims 47 to 49, characterized in that a force accumulator ( 357 ) is provided between the side legs ( 353 , 354 ) of the guide bracket ( 349 ) and the arms ( 328 ). 51. Device according to claim 50, characterized in that the energy accumulator ( 357 ) are formed by an elastic material such as rubber. 52. Device according to at least one of the preceding claims, characterized in that between the flange ( 29 , 129 ) and the second flywheel ( 4 , 104 ) stops ( 39 , 139 ) for limiting the angular deflection of the first damping device ( 13 , 113 ) are provided. 53. Device according to claim 52, characterized in that the stops are formed by spacer bolts ( 39 , 139 ) which on the one hand the disks ( 37 , 38 ; 137 , 138 ) of the first damping device ( 13 , 113 ) with each other and on the other hand with the second Connect the flywheel ( 4 , 104 ) and project axially through cutouts ( 44 ) in the flange ( 29 , 129 ). 54. Device according to claim 53, characterized in that the rotation angle of the first damping device ( 13 , 113 ) is limited by the stop of the spacer bolts ( 39 , 139 ) at the end regions of the cutouts ( 44 ) in the flange ( 29 , 129 ). 55. Device according to one of claims 52 to 54, characterized in that the flange ( 29 ) on its inner periphery has radial teeth ( 45 ) which engage between the stud bolts ( 39 ). 56. Device according to claim 55, characterized in that the teeth ( 45 ) are formed by introducing cutouts ( 44 ) into the radially inner regions of the flange ( 29 ). 57. Device according to at least one of the preceding claims, characterized in that the flange ( 29 , 129 , 229 , 329 , 429 , 529 , 629 ) can be rotated to a limited extent with respect to the second flywheel ( 4 , 104 ). 58. Device according to one of claims 1 to 57, characterized in that the disks ( 424 , 425 ) of the further damping device ( 414 ) are axially fixed to one another via spacing means ( 455 ), such as spacing bolts, and at least one ( 425 ) of the disks ( 424 , 425 ) between the spacing means ( 455 ) has a circumferentially resiliently preloaded corrugation ( 425 a) which braces the flange ( 429 ) in the direction of the other disk ( 424 ). 59. Device according to claim 58, characterized in that the spacer bolts ( 455 ) serve at the same time for fastening the disc ben ( 424 , 425 ) on one ( 403 ) of the flywheels. 60. A device according to at least one of the preceding claims, characterized in that the washers ( 524 , 525 ) provided on both sides of the flange ( 529 ) of the further damping device ( 514 ) by means of spring clips ( 530 ) or clamps distributed over the circumference against the Flange ( 529 ) are clamped. 61. Device according to claim 60, characterized in that the brackets or brackets ( 530 ) axially overlap the flange ( 529 ) and the two disks ( 524 , 525 ) of the further damping device ( 514 ) and with radially extending legs ( 530 a, 530 b) reach behind the washers ( 524 , 525 ) axially and apply them in the direction of the flange ( 529 ). 62. Device according to at least one of the preceding claims, characterized in that one ( 503 ) of the centrifugal masses has axial projections ( 555 ) which fit into cutouts ( 555 a, 555 b) of the disks ( 524 , 525 ) flanking the flange ( 529 ) ) of the further damping device ( 514 ) intervene to secure it against rotation. 63. Device according to claim 62, characterized in that - viewed in the circumferential direction - between the axial projections ( 555 ) on the circumference of the flange ( 529 ) integrally formed from casual ( 528 ) engage radially and energy accumulator ( 535 ) in recesses ( 533 , 534 ) the discs ( 524 , 525 ) of the further damping device ( 514 ) are added, which serve as an end stop for limiting the angle of rotation of the further damping device for the arms ( 528 ) of the flange ( 529 ). 64. Device according to one of claims 62 or 63, characterized in that at least individual recesses ( 534 ) for receiving the energy accumulator ( 535 ) of one disc ( 525 ) relative to the axially opposite recesses ( 533 ) of the other disc ( 524 ) in The circumferential direction is offset in such a way that the energy accumulators ( 535 ) accommodated in the axially opposite recesses ( 533 , 534 ), the disks ( 524 , 525 ) against those protruding through the cutouts ( 555 a, 555 b) of the disks ( 524 , 525 ) Brace the protrusions ( 555 ) in the circumferential direction. 65. Device according to one of claims 62 to 64, characterized in that the axial projections are formed by bolts ( 555 ) or pins which are attached to one ( 503 ) of the momentum. 66. Device according to at least one of the preceding claims, characterized in that the flange ( 629 ) in the region between the disks ( 624 , 625 ) of the further damping device ( 614 ) has axial recesses ( 656 , 657 ) in which tear pads ( 658 , 659 ) are accommodated , which are clamped between the disks ( 624 , 625 ) of the further damping device ( 614 ). 67. Device according to claim 66, characterized in that the Recesses are axially continuous and through them in each case a friction block with a greater thickness than that of the flange extends through. 68. Device according to claim 66 or 67, characterized in that the friction blocks ( 658 ) are axially displaceable in their recesses ( 656 ), but are guided in the radial and / or circumferential direction. 69. Device according to one of claims 66 to 68, characterized in that the axial recesses ( 656 , 657 ) receive a pair of friction blocks arranged in series ( 658 , 659 ), between which a force accumulator, such as. B. a plate spring ( 663 ) is provided, which braces the friction blocks ( 658 , 659 ) against the discs ( 624 , 625 ) of the further damping device ( 614 ). 70. Device according to claim 69, characterized in that the pair of friction blocks ( 658 , 659 ) and the intermediate energy store ( 663 ) are axially held together by connecting means ( 662 ), but the connecting means ( 662 ) have a limited axial displacement of the two Allow friction blocks ( 658 , 659 ) to each other, against the action of the energy accumulator ( 663 ). 71. Device according to one of claims 66 and 68 to 70, characterized in that the flange ( 629 ) has axially directed blind holes ( 656 , 657 ) for receiving friction blocks ( 658 , 659 ), the axially between each towards each other directed blind holes ( 656 , 657 ) existing partition ( 660 ) of the flanges cal ( 629 ) has an opening ( 661 ) through which a, the pair of axially opposite friction blocks ( 658 , 659 ) holding together connecting means ( 662 ) protrudes, wherein between at least one (658) of the friction blocks ( 658 , 659 ) and the intermediate wall ( 660 ) a force store, such as a plate spring ( 663 ) is arranged, the friction blocks ( 658 , 659 ) between the disks ( 624 , 625 ) of the further damping device ( 614 ) and furthermore the connecting means ( 662 ) prevent a limited axial displacement of the opposing friction blocks ( 658 , 659 ) d he effect of the energy accumulator ( 663 ). 72. Device according to one of claims 1 to 71, characterized in that the first damping device ( 13 , 113 ) is provided radially within the further damping device ( 14 , 114 , 214 , 314 , 414 , 514 , 614 ).