GB2315316A - Torque transfer apparatus - Google Patents

Torque transfer apparatus Download PDF

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Publication number
GB2315316A
GB2315316A GB9722621A GB9722621A GB2315316A GB 2315316 A GB2315316 A GB 2315316A GB 9722621 A GB9722621 A GB 9722621A GB 9722621 A GB9722621 A GB 9722621A GB 2315316 A GB2315316 A GB 2315316A
Authority
GB
United Kingdom
Prior art keywords
flywheel mass
flywheel
mass
component
damper
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB9722621A
Other versions
GB2315316B (en
GB9722621D0 (en
Inventor
Lamellen & Kupplungsbau Luk
Wolfgang Reik
Robert Felger
Albert Albers
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
LuK Lamellen und Kupplungsbau GmbH
Original Assignee
LuK Lamellen und Kupplungsbau GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by LuK Lamellen und Kupplungsbau GmbH filed Critical LuK Lamellen und Kupplungsbau GmbH
Priority claimed from GB9712813A external-priority patent/GB2312945B/en
Publication of GB9722621D0 publication Critical patent/GB9722621D0/en
Publication of GB2315316A publication Critical patent/GB2315316A/en
Application granted granted Critical
Publication of GB2315316B publication Critical patent/GB2315316B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/10Suppression of vibrations in rotating systems by making use of members moving with the system
    • F16F15/12Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon
    • F16F15/131Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon the rotating system comprising two or more gyratory masses
    • F16F15/139Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon the rotating system comprising two or more gyratory masses characterised by friction-damping means
    • F16F15/1397Overload protection, i.e. means for limiting torque
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F1/00Springs
    • F16F1/02Springs made of steel or other material having low internal friction; Wound, torsion, leaf, cup, ring or the like springs, the material of the spring not being relevant
    • F16F1/32Belleville-type springs
    • F16F1/324Belleville-type springs characterised by having tongues or arms directed in a generally radial direction, i.e. diaphragm-type springs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/10Suppression of vibrations in rotating systems by making use of members moving with the system
    • F16F15/12Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon
    • F16F15/131Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon the rotating system comprising two or more gyratory masses
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/10Suppression of vibrations in rotating systems by making use of members moving with the system
    • F16F15/12Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon
    • F16F15/131Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon the rotating system comprising two or more gyratory masses
    • F16F15/13142Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon the rotating system comprising two or more gyratory masses characterised by the method of assembly, production or treatment
    • F16F15/1315Multi-part primary or secondary masses, e.g. assembled from pieces of sheet steel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/10Suppression of vibrations in rotating systems by making use of members moving with the system
    • F16F15/12Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon
    • F16F15/131Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon the rotating system comprising two or more gyratory masses
    • F16F15/13164Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon the rotating system comprising two or more gyratory masses characterised by the supporting arrangement of the damper unit
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D13/00Friction clutches
    • F16D13/58Details
    • F16D13/70Pressure members, e.g. pressure plates, for clutch-plates or lamellae; Guiding arrangements for pressure members
    • F16D2013/703Pressure members, e.g. pressure plates, for clutch-plates or lamellae; Guiding arrangements for pressure members the pressure plate on the flywheel side is combined with a damper
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D13/00Friction clutches
    • F16D13/58Details
    • F16D13/70Pressure members, e.g. pressure plates, for clutch-plates or lamellae; Guiding arrangements for pressure members
    • F16D2013/706Pressure members, e.g. pressure plates, for clutch-plates or lamellae; Guiding arrangements for pressure members the axially movable pressure plate is supported by leaf springs

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Mechanical Operated Clutches (AREA)

Abstract

In torque transfer apparatus a first flywheel mass 2, 502 connectible with a rotary output element such as the output shaft of an engine is rotatable with as well as relative to a second flywheel mass 3, 503 connectible to a rotary input element. Relative rotation between the masses 2, 3; 502, 503 is opposed by a damper 9 which has energy storing means 10 acting in a circumferential direction. The first flywheel mass comprises a disc-like component 13 and has an axial projection 22 extending from the radially outer part of that component in the direction of the second flywheel mass. A starter gear ring 20 is fixed to the first flywheel mass. The first flywheel mass 2 has radially inwardly positioned securing means 7 for securing the flywheel mass to a rotary output element, and the disc-like component 13 has openings 563 radially outside the energy storing means 10 for fastening the second flywheel mass 503 to a cover plate by means of fastenings 503a which are accessible through the openings.

Description

Toraue transfer apparatus The invention concerns a torque transfer apparatus, with at least two flywheel masses, rotatable relative to one another through a bearing against the action of a damping device with energy accumulators acting in a circur-rerential direction. Of the flywheels one (the primary flywheel mass) may be attached to the driven shaft of a combustion engine, and another (the secondary flywheel mass) may be connected to the input shaft of a gear box through a friction clutch.
The purpose of the above invention is to make torque trans er devices which are distinguished by their small size both in axial and radial directions. Furthermore, the an of the invention is to increase the life span of this -ype of torque transfer device and thus enable the device to have reliable applicaticns such as in motor vehicles.
A further fundamental aim of the invention is to allow the torque transfer device to be fastened to the output shaft of a combustion engine as easily as possible. Also, both reasonably inexpensive and economical production and assembly, as well as a simpler and faster method of replacement (for example when renewing worn components), should make this kind of torque transfer device possible.
Moreover, these devices, with a range of various different types, should open the way to making the largest possible effective diameter for the friction clutch and should keep the c;-erall dimensions of the whole unit down by using just ne requisite diameter. This would mean that this kind - torque transfer device could be used even where space was severely restricted, for instance in vehicles with a built-in transverse front engine.
In addition, an objective of the invention is to reduce the number of individual components and also to save on the natural resources by using the smallest amount of materials possible and by making the least amount of waste possible. The environment may also be helped by a reduction in the manufacturing processes, by making savings on energy and by cutting down on production extras which have been used up until now.
A further aim of the invention is to protect the components of the torque transfer device from the effects of extreme forces and thus to prevent any of these extreme fores being passed on to the downstream gear box of the torque transfer device or into the drive train.
According to the invention, there is provided apparatus for transmitting torque, comprising a first flywheel mass connectable with a rotary output element; a second flywheel mass rotatable with as well as relative to the first flywheel mass about a common axis and connectable witri a rotary input element; and means for opposing rotation of said flywheel masses relative to each other including at least one damper having energy storing means acting in a circumferential direction of said flywheel masses, said at least one damper constituting a torque path between said flywheel masses wherein the first flywheel mass comprises a disc-like component which has an axial projection extending from the radially outer part of the component in the direction of the second flywheel mass, and a starter gear ring, and has radially inwardly positioned securing means for securing the flywheel mass to m rotary output element and the disc-like component has openings radially outside the energy storing means for fastening the second flywheel mass by means of fastenings whch are accessible through the openings.
In a second aspect, the invention provides apparatus for transmitting torque comprising a first flywheel mass connectable with a drive and a second flywheel mass connectable with the first flywheel mass through a torsion vibration damper, the second flywheel r:ss being rotatable relative to the first flywheel mass and the clutch housing of a friction clutch being fitted on the second flywheel mass, the friction clutch having a rotationally fixed but axially displaceable pressure plate, an energy storing means, such as a diaphragm spring, biasing the pressure plate and a clutch disc arranged between the pressure plate and a counter pressure plate, wherein at least the counter pressure plate (which forms a component of the second razz lywheel mass), the clutch cisc, the pressure plate, tne clutch housing and the energy storing means form a reassembled unit which is connectable as such by means of fasteners with a component provided on the first flywheel mass, wherein the first flywheel mass has openings through which the fastenings can be tightened from the side of the first flywheel mass facing away from the second flywheel mass.
The first flywheel mass can be a sheet metal part, and the securing means can be openings for receiving threaded fasteners.
The fastenings for the second flywheel mass are preferably accessible from the side of the first ywheel mass facing away fre the second flywheel mass trough the openings and into the second flywheel mass.
The second flywheel mass can be connectable through an engageable and disengageable friction clutch with a rotary input element.
Between the two flywheel masses, at least one hysteresis device can be provided which is arranged radially outside the longitudinal axis of the energy storing means of the damper which acts between the two flywheel masses.
The axial projection of the first flywheel mass can be fo=.ed by an annular inertia ring which is fastened at the radially outer region of the flange like component. The inertia ring can be made as a folded plate and, when considered in cross-section can be angularly formed. The inertia ring can carry the starter ring gear.
The damper can have an input part, rotationally connected with the first flywheel mass, as well as an output part rotationally connected with the second flywheel mass, wherein the rotational connection between the damper input part and the first flywheel mass lies radially inside the energy storing means of the damper, and the connection between the output-part of the second flywheel is provided radially outside the energy storing means.
The two flywheel masses as well as the friction clutch carried by the second flywheel mass preferably form one constructional unit. The fastening means for connecting the first flywheel mass with the rotary output element can be integrated in the apparatus so that they are secured agaInst loss.
A component of the damper which is biased by the energy storage means can serve as a bearing between the two fly.çheel masses, and the component can have openings for receiving fastenings.
The friction clutch carried by the second flywheel mass can have a diaphragm spring with radially inwardly directed tongues, and in the region of the tongues and/or in the regIon between the tongues, openings are provided for tightenIng of fasteners. Openings fcr tightening of fastenings can also be provided in a component of the clutch disc.
A torque transfer device in accordance with the invention can be provided in an advantageous manner with a friction clutch as a so-called compressed clutch, or equally with the friction clutch as a so-called pulled clutch.
With the aid of the Figures, the invention will be described Fn more detail.
Figure 1 is a simplified sectional drawing through a torcle transfer device according to the invention; Figure 2 is an enlarged drawing of part of Figure 1; Figure 3 shows a design variant of a torque transfer device in accordance with the invention; and Figures 4 to 9 show further variants of a torque transfer device in accordance with the invention.
Figure 1 shows part of a flywheel in halves 1 (the original design of which is described in different versions i the German patent applications P 43 20 381 and P 43 11 90=) to which particular reference is made here and the content of which is incorporated y reference into part of the following description. This ype of flywheel 1 comprises a first or primary flywheel rass 2, which can be attache to a crankshaft of a combustion engine (not shown), ani a second or secondary flywheel mass 3. A friction clutch 4 is fixed on this secondary flywheel mass 3 with a clutch disc 5 located between, through which a gear bcx (also not shown) can be connected or disconnected. This clutch disc 5 is clearly shown and is merely n example. It can take other structural forms containIng the friction and/or damping elements, or can even be equipped with a spring cover.
In this case the flywheel masses 2 and 3 are journalled relative to one another by a bearing 6 with the interposition of components connected firmly to them. The bearing in this example is positioned radially within bores 7 or the introduction of fixing screws 8, allowing the assembly of the first flywheel ,=sus 2 or the whole torque transfer device 1 onto the driven shaft of the combustion engine. The single-row ball bearing 6 shown has a sealing cap 6a with a lubricant chamber, so that the sealing cap 6a also serves as a thermal isolator, so reducing the heat transfer from the second flywheel mass 3 to the bearing 6, and/or prevent a thermal bridge.
Between the two flywheel masses 2 and 3 is a damping device 9 which in this instance acts on helical compression springs 10, which themselves are positioned in an annular space 11 forming a roughly torus-shaped space 12. The helical springs 10 which are shown and used in this instance can be replaced by stably constructed alternative energy accumulators or Ly leg springs for example. The annular space 11 is therefore filled with a dry l-ibricant (such as graphite powder or something similar), or with a thick viscous material (such as oil or grease).
The primary flywheel mass 2 contains a component 13, preferably made or drawn from sheet etal, which serves to connect the first flywheel mass 2 or the whole of the divided flywheel 1 to the output shaft of the combustion engine or to a shaft connected thereto. The component 13 forms a flange-like region 14 extending essentially in a radial direction which carries radially inwardly a flange 15. This flange 15 has areas lSa extendin in a radial direction with recesses 7, aligned bores or openings for the fixing screws 8. The single roller bearding 6 is fixed with its inner ring 16 to an outer casing or shoulderpiece in the axial end-section 15b of flange 15. The second flywheel mass 3 is supported on the outer ring 17 of the roller bearing of bearing 6.
The radial piece 14 extends radially outwards and passes into a shaped area 18 on the axial side of the combustion engine, which then extends radially outwards itself and forms the starter gear ring 19. Thus the starter gear ring 19, in the outer radial area of the component 13 with deformed and bent material, has its wall on the outer radial section of the housing 13, but wit its limb 20 pointing radially inwards. The shaping ar--/or teeth of the starter gear ring can be formed after the folding of the plate into this shaped metal part. This shaping can be made by cutting processes such as milling or broaching.
The shaping c- the starter gear ring 19 can also be made by embossing or by using a material flow production process, or e7en by being pressed out. Another possible manufacturing process for this shaping uses high energy light rays such as lasers to cut them out. It is useful if the sections of metal used at least i--- the shaping and/or teeth =f the starter gear ring 19 are stronger than those used i other regions. Such a partial increase in strength can for example be achieved by inductive strengthenin or by case hardening.
To increase the angular momentum of the twin mass flywheel 1 which rotates around its axis, the primary flywheel mass 2 which can be connected to a combustion engine has an inertia ring 21. The inertia ring 21 is made out of a plate boo."" and has one limb 22 pointing in an axial direction and two limbs 23 and 24 pointing in a radial direction, so that the inertia ring 21 has an approximately L-shaped cross-section. The inertia ring 21 is mac by folding or bending a piece of metal which is originally straight in its cross-section, as described for example in the German patent application P 43 15 209, which is particularly referred to both here and in connection with the starter gear ring 19, and which in this resect forms at least part of the present application.
The limb 22 stretching in an axial direction butts onto limb 20, which also extends in an axial direction, of the starter gear ring 19 with impingement region 25. By such manufacture of the inertia ring, its shape can be fitted for example to the internal shape of the housing containin the twin-mass flywheel, such as the gearbox bell housing so that no movement can t ke place.
The free end of limb 22, which stretches in an axial direction, extends away from the combustion engine and by forming eIther a bend or curve 22a into the radially extending limb 24 of the inertia ring 21. The inertia ring 21 thus butts onto the side (which is opposite to the combustion engine) of pot-like region 18 of the first flywheel mass 2, with this curve 22a and the radial limb 24. Radially within this area limb 24 points in the direction of the secondary flywheel mass 3 towards an axially offset section 24a, which has its wall touching the wall of the second limb 23 extending in a radial direction. Limb 23 rises above secticn 24a outwards in a radial direction, and ends at a radial distance from the axially extending limb 22. In the region of curve 22a the inertia ring 21 is firmly connected to the primary flywheel mass 2 by way of several welds 27, which are spread over te perimeter and which are in recesses 26.
Flange 15 is connected centrally to the first flywheel mass 2. It can be centred by using a centering seat 28, for example, which combines with the central recess in section 13. Otherwise the centering, and if necessary the connection, of flange 15 to the first flywheel mass 2 can be achieved by using lugs which can be passed through from the side opposite the combustion engine for example, using part of flange 15. Flange 15 also extends radially inwards to centering seat 29 which helps to centre the split flywheel 1, for example on an engine crankshaft.
Outside its radial area 15a the flange 15 extends radially outwards from the side with the combustion engine so as to reach back into its outer radial area in a radial direction. Inside this outer radial area flange 15 has a second flange 30 firmly attached to it. This connection can result from the drawing of material from flange 15 to make connection lugs. Within this connectIon flange 30 extends both radially and inwards so that a slight cavity 31 is visible on the side with the combustion engine.
Flange 30 extends radially within the cavity 31 over the combustion engine to region 32, which itself extends inwards towards area 33. The radial region 33 touches radial piece ISa of flange 15 and has, like the flange, recesses for the introduction of fixing scree 8, when the side of radial region 33 facing away from the combustion engine can comprise an abutment for the heads of the fixing screws 8.
In the outer radial area and the area of cavity 31 flanges 15 and 30 form impingement regions 34 and 35 for the energy acc;rulators in the form of helical springs 10. The impingement regions 34 and 35 are formed by radial extension arms 15c and 31c, which project into the areas in between the circumferentially acting energy accumulators 10. The extension arms 15c and 31c, along with their impingement regions 34 and 35, are made so that they fit the spring ends of energy accumIators 10. The ends of the springs cooperative with the impingement regions 34 and 35 might only show a point of separation and may perhaps neither be positioned on the above springs, nor have their ends vertically touching the central spring axis. This means that the end coils of energy accmulators 10 actually correspond with any of the other coils inside the energy accumulators 10, and so are shown to be comparable to a screw with practically the same gradient. Thus it is possible for these end coils to be fitted as sprung coils, so that any non-sprung coils are not used and so that both greater spring capacity and smaller actual lengths of spring can be used. By utilising this arrangement of spring coils the spring wire itself must be cut and thus the other operations (for example the positioning of the last spring coil onto the one immediately preceding it, and the rinsing of the spring end so that it touches one of the flat abutment surfaces) can be left out.
This type of spring arrangement confined with the requisite irrrpingement regions is not limited purely to the example of a twin mass flywheel as give above, but can be used In all other combinations, such as with dampers.
Likewise i is possible to replace both flanges 15 and 30 with just one piece, for example a so erred or forged piece, wherein again the impingement regions 34 and 35 can be fitted to the energy accumulators 10.
The two flanges 15 and 30, or indeed one of the replacement intered or forged pieces, can be made in such a way that they form an additional torsional protector in the impingement areas 34 and 35 of the energy accumulators 10 to prevent the elements 10. Such a torsional protector makes sure that the energy accumulators stay exactly in their original specified position and are unable to turn around their coil axis, for example. This has the advantage that the free spring end coil is always at the same place on the impingement regions 34 and 35, and thus it ensures that the end coils with all their spring properties and volumes are made available to absorb any vibration.
The energy accumulators 10 are supported on the other hand on impingement regions 36 and 37. The energy storage element impingement regions 36 are arranged on a first cover plate 38 which is supported radially inside on bearing 6 and/or here on the outer bearing ring 17 of the roller bearing 6, and which radial outwardly supports the secondary flywheel mass 3.
In addition, in its inner radial area the cover plate 38 has a shoulder 39, which extends axially to the engine, and which has an inner diameter able to accommcdate the outer bearing ring 17 combined with the seal cap Ea. This shoulder has a diameter restriction 40 on the side opposite to the combustion engine, which serves as an axial stop or fixture between cover plate 38 arn roller bearing 6. Cover plate 38 extends radially inclined outwards from the cross-section restriction 40 and away from the combustion engine, and this section 41 extends substantially straight.
The straight section 41 contains access recesses 42 which are designed to take the heads of the ixing screws 8, and, in se doing, to fix the screws ^ in a co-axial position on the rotation axis of the twFn mass flywheel 1, when the torque transfer device is in neither a fitted nor an installed condition. The straIght cover piece section 41 leads radially outwards into area 43 (which is a segment of a circle in cross-section), which is at least substantially conforming to the outer edge of energy storage element 10 and which partly surrounds it axially and radially. A radial piece 44 is connected on to the free combustion engine end of region 43 pointing radially outwards, and is firmly fixed by means of radial piece 45 of the second cover plate 46, which is itself in an axial position between cover plate 38 and the retal housing 13.
The two cower plates 38 and 46 are sealed radially by means of a O-ring 47.
The cover plate 46 partly contains the O-ring 47 radially within the radial piece 45 and extends axially away from the side or which the combustion engine is placed into the space contained by cover plate 38. Thus the seal of the ring-shaped chamber 11 and the space 12 is ensured, whilst at the same time cover plates 38 and 46 are both centred to each other. From this point cover plate 46 runs substantially radially inwards and substantially conforms to the outer contour of the energy storage element 10, and it is also extended into the axial housing between the plate part 13 of the first flywheel mass 2 and the flange 15.
Radially within impingement regions 37 cover plate 46 has a region 5 axially facing the combustion engine, on which plate spring 49 lies. Plate spring 49 ma. < es inner radial contact with flange 15, and so forms an inner radial seal for chamber 11. Therefore plate spring 49 can be centred both in the region of cover plate 46 as well as to flange 15. Another plate spring 50 makes a seal for chamber 11 on the inner radial between the flange 30 and the cover plate 38. At this point the outer diameter of plate spring 50 touches the projection 31 of flange 30, and the inner diameter touches cover plate 38 in the region of piece 32 which runs axially from flange 30. To allow plate spring 50 to be centred, cover plate 38 has several centering projections 51 spread around its perimeter which are partially interspersed with material from cover plate 38. Instead of several centering shoulders 51 arranged around the perimeter, it is also possible to use one completely circular piece, or even to centre plate spring 50 relative to the flange 30.
In the region of its outer diameter, the cover plate 46 carries the second flywheel mass 3. To this end the cover plate 46 has an extended radial region 45 which extends over the secondary flywheel mass 3 in a radial direction and becomes at its outer radial end one of the axial regions 45a, which points away from the combustion engine.
Cover plate 46 at least partly covers the secondary flywheel mass 3 in an axial direction with this axial area 45a, and it forms a connecting region on the side opposite to the combustion engine, which has yet to be described.
In the inner radial region of the secondary flywheel mass 3 the cover plate 46 has tongues 46a pointing away from the combustion engine in an axial direction, penetrating radial region 44 of cover plate 38 and which are plastically shaped after the assembly of these pieces so that they point radially inwards on the side of the secondary flywheel mass 3 to firmly connect the plate 46 to the cover plate 38. These tongues 46a are made directly out of the material of cover plate 46, so that an additional flanged metal plate can be dispensed with.
Another advantage of this construction can re seen by the reduced heat transfer from the secondary flywheel mass 3 to both cover plates 38 and 46, thus reducing in turn the direct effect on the lubricant. In addition, recesses 45b, in radial region 45 and in a conical extension of cover plate 46, help the cooling effect. radial regions 45 and 46 are positioned on the side of the secondary flywheel mass 3 (and opposite to the friction surface), so that if a leak should ever occur or if o-ring 47 should fail then the medium or lubricant contained in chamber 11 is guided towards primary flywheel mass 2. This stops the effective friction on the linings of clutch disc 5 from being impaired, and so allows the friction clutch 4 to continue to transmit the full torque.
As well as the clutch unit (consisting of clutch 4 and clutch disc 5), the twin mass flywheel 1 also forms a unit which is pre-assembled, which is shipped and journalled, and can be mounted both easily and raticnally on the crankshaft o a combustion engine. This configuration then allows various processes to be dispensed with such as the otherwise necessary centering of the clutch disc, the processes of positioning the clutch disc and connecting the clutch, the introduction of the centering mandrel, the centering of the clutch disc itself, as well as the insertion of the screws, the screwing on of the clutch and the removal of the mandrel.
Fixing screws 8 can be already mounted and positioned in the drill holes of flange region 14 and flange 15 so that they are effectively kept in a secure position, for example by resilient means, which are dimensioned so that their holding force will be overcome when the screws 8 are tightened.
Clutch disc 5 is clamped in a precentred position between pressure plate 52 and the friction surface of the secondary flywheel mass 3 on a rotational axis of the unit. It is in such a position that the holes 53 designed in clutch disc 5 are arranged in such a way shat they allow a screwing-up tool to be used when mounting the whole section or unit onto the driven shaft of a combustion engine. Also, and as can be seen in the various configurations in the drawings, the holes 53 may be smaller than the heads of the fixing screws 8 so that the screws 8 are kept both correctly in position and securely within the unit.
Plate spring 54 also has cutouts or holes for the passage of a screwing-up tool in its torques 54a, which are not shown in this Figure. These cutouts can form widenings or lengthenings of the slots which exist between the tongues 54a. The openings in plate spring 5A and the holes 53 in clutch disc 5 cover each other in the direction of the axis, and therefore their axially aligned positioning allows access to an assembly tool for tightening the screws 8 and for fixing the whole unit onto the crankshaft of a combustion engine.
Above plate spring 54 the actuable friction clutch 4 has a pivot bearing 55 on the cover side of the clutch cover 57 and a pivot bearing 56 on the opposite side of the clutch cover 57. Pivot bearings 55 and 56 are formed by wire rings and are held by plates 58 divided at the circumference. The plates 58 are made in one piece with the cover 57, and are made out of the same, but necessarily shaped, material. On the side opposite to cover 57 the plates 58 at least partly grip the pivot bearing 56 both in axial and radial directions. The connection of pivot bearing 55 radially outside the pivot bearing 55 is ensued by a pressed-in swage 55 in cover 57. Instead of one continuous closed swage 55, several discrete swages can be used if spread around the perimeter. Pressure plate 52, as is shown in the drawings, can at least be fitted in the region of the edges of plates 38 and also in the other regions at the edge of pivot bearing 56. However, as an alternative to the given example, it can also be useful to leave the matching of the plates 61 constant around tune whole perimeter.
Leaf spring elements 60 are used for both the torque transfer and for the lifting movement of pressure plate 52. They are connected on one side to the housIng or the cover 57 via rivets which are not shown here, and on the other side to pressure plate 52 via rivets 51. The rivetting on pressure plate 52 occurs at pressure plate cams 62 which in this example jut inwards and which are positioned radially inside the friction surfaces of clutch disc 5. Pressure plate cams 62 penetrate plate springs 52 in an axial direction and in the recessed sections so that the leaf spring elements 60 are positioned on the side of cover 57 opposite to the pressure plate 52. This type of leaf spring arrangement is not limited to a divided flywheel, but can also be used with other types of clutches, such as with a conventional flywheel. The necessary recessed sections in the plate spring can be made by removing parts of the plate spring tony yes 54a or even by removing complete spring tongues 54a. The plate spring tongues 34a are shaped to fit the ede of the support of the clutch disc 5 and run alongside and parallel to it for this example pressured clutch construction, with friction clutch 4 in a disengaged position.
Alongside the recesses 42 in cover plates 38 and 53 of clutch disc 5 further openings or passages can be made which can help to cool the whole unit - in the region of clutch covers 57 and 5a in clutch disc 5, or in the secondary flywheel mass 3 and 63, and in section 13 o the primary flywheel mass 3. If the whole unit is sufficiently cooled then, amongst other things, this should prevent any of the thick material (eg grease) contained in the torus-shaped area 12 from being excessively heated, which would thus lower its viscosity and cause it to flow. Moreover, an increased thermal load negatively affects the life span of the whole unit. To further improve the elimination of any heat, the surfaces of the secondary flywheel mass 3 and/or in pressure plate 52 can be enlarged, so that they, and the passages already described, can be shaped like a compressor blade.
The clutch cover 57, which is at least indirectly connected to the secondary flywheel mass 3, consists essentially of an axial region 64 which is shaped generally as a hollow cylinder, and of the section 65 which at least begins by running radially and in the region of which the plate spring 54 is pivoted. The axial region 64 points towards the combustion engine and has a connecting piece at its free end, which has yet to be described.
Figure 2 is an enlarged and detailed section of Figure 1 and shows the disengageable connection 66 between axial region 64 of clutch cover 57 and axial piece 45a of cover plate 46. This connection 66 fulfils two purposes.
Firstly, with the help of this connection 66, it is possible for example to dismantle without damage the whole unit - comprising the divided flywheel 1 and the clutch joined onto it - in order to replace clutch disc 5 and, having replaced the worn parts, to easily reassemble it.
Secondly, connection 66 serves as a sliding clutch and so protects the whole unit and the downstream drive train from excessive torque loads and over momentum which would otherwise lead to an increased load on either the whole drive train or at least on certain parts of it, if not to their complete destruction.
The axial region 64 of the cover 57 has a radial collar 67 at its end facing the combustion engine, which has two curved regions 68 and 69 running in opposite directions.
The axial piece 45a of the cover plate 46, which also acts as a support for the secondary flywheel mass 3, is widened in the diameter facing away from the combustion engine (and connects in an axial direction to limb 22 of inertia ring 21), engages radially around collar 67 with axial section 70 and covers the outer periphery in an axial direction. A tongue region 71 is connected to this axial section 70, which is curved and which has its end 72 facing radially. Therefore tongues 71 and recesses 73 alternate around the edge of the cover plate and support 46, as well as on collar 67 of the clutch cover 64. This collar 67 has teeth 74 pointing outwards on its outer radial region. These teeth 74 alternate with recesses 75 around the edge so that the recesses 75 are bordered inwards, as represented by the dotted line 76. Tongues 71 are thus extended less in the direction of the perimeter than are the recessed sections 75, and the edges of teeth 74 are extended less than those of the recessed sections 73. Furthermore, the inner diameter of the tongue region 71 (at the end 72 pointing inwards) is greater than the outer diameter of collar 67 at point 76 of the recessed sections 75. This configuration ensures that clutch cover 57 and support 46 penetrate in the region of the connection 66 axially, so that they can be fitted together.
On its inner radial curved region 6= the collar 67 partly surrc nds an undulating spring 77, which is shown to have a circular cross-section. This undulating ring or spring 77 is supported in a groove 78 of the secondary flywheel mass 3. On its other side the collar 67 partly surrounds a wire ring 79 with its outer radial curved region 69.
The wire ring 79 is in turn supported on the tongues 71 of support 46. Wire ring 79 is open, when viewed around its perimeter, and its ends 80 which originally faced each other are bent in such a way that they point axially away from the combustion engine at an angle of approximately 90 degrees to the plane of the wire ring 79 . Moreover, these bent-over ends 80 enter support 46 in the region of the recessed sections 73 between the tongues 71, so that the wire ring 79 is protected from any twisting relative to the cover plate 46.
When it is assembled the secondary flywheel mass 3 is positIoned in the body formed by axial piece 45a, and cover plate 46 is already fitted with damping device 9 on the primary flywheel mass. After positioning the clutch disc 5 and the undulating spring 77, the clutch cover 57 is te be slid with the mounted pressure plate 52 and plate spring 54 into the area of tongues 71 or with teeth 74 axially towards the combustion engine, so that collar 67 lies closer to the combustion engine than tongues 71 when viewed axially. In this process both the undulating spring 77 and the plate spring 54 are pretensioned and they exert an axial force which after insertion of the wire ring 79 and thus making of the connection 66 is taken up b the wire ring 79, as the secondary flywheel mass 3 is supported on its side facing the combustion engine by radial piece 45 of cover plate 46.
When engaged in this configuration the axial energies of plate spring 54 and undulating spring 77 are added together, whereas when it is disengaged only the axial energy of the undulating spring 77 is applied. Should the need arise, undulating spring 77 can besides exert a low radial force, so facilitating the centering of the secondary flywheel mass 3 and which also helps to prevent it from falling out of the body formed by axial piece 45a.
To make assembly easier, plate spring 54 can be tensioned, and thus kept in a "disengaged position", so that during assembly only the spring force of the undulating spring or ring 77 has to be surmounted.
In order to dismantle the unit it is only necessary to apply axial energy again so that the spring force of the plate spring 54 and of the undulating spring 77 is overcome, which releases the connection 66 and then allows the wire ring 79 simply to be removed. At this point all that is needed is to move the offset ends 80 relative to each other by using a pair of pliers or something similar, so that the diameter of the wire ring 79 is reduced. The wire ring can then be removed and then the teeth 74 can be moved again through the recesses 73.
In the assembly method described here, none of the parts - the secondary flywheel mass 3, the clutch 4 or clutch disc with the support 46 - are interlocked in any way.
The frictionally engaged connection as shown here forms a slip clutch with the friction surfaces 81 between the secondary flywheel mass 3 and the support 46, and the surfaces 82 between the collar 67 and the wire ring 79.
In this configuration therefore the whole friction clutch 4 along with the secondary flywheel mass 3 can be moved in a circumferential direction in relation to the rest of the twin mass flywheel 1 so that any transmission of excessive torsional shocks is hindered from passing to the rest cf the drive train. The load transfer ability of this slip clutch is determined by the spring rate of the plate spring 54 and the undulating spring 77 in addition to the choice of friction pairings on the friction surfaces 81 and 82, so that at these points friction linings can also be positioned.
Figure 3 contains components which match or are similar to those parts already described, and which have similar numbers, but which are increased by 100.
The divided flywheel 101 corresponds in the original design with the twin-mass flywheel 1 already described, but has a disengageable 166 of a different design. Thus at the free end of its axial region 145a the support plate 146 forms a collar 145c pointing radially outwards, which in turn has teeth 171 and recessed sections 173 spread around its perimeter. This radial collar 145c is surrounded radially and projected axially by the axial piece 164 of clutch cover 157, which itself has tongues 174 pointing inwards, whilst being spread around the perimeter and alternating with recessed sections 175. The assembly and locking in the region c connection 166 occur in a similar way to that already described, so that undulating spring 177 is positioned in an axial direction between the collar 145c and the clutch cover 157, and so that he wire ring 179 is fitted between the flange 145c and the tongues 174 which point inwards. In this confi-uration the angled ends 180 of the wire ring 179 point towards the combustion engine.
In order to position the secondary flywheel mass 103 in the pot of the support plate 146 formed by the axial piece l4a, a further undulating spring 183 is designed, which is radially pretensioned. Here the slip clutch has friction surfaces 181, 182a and 182b. On the friction surface 181 there is frictional force which is proportional to the pressure of the plate spring 154, and on the friction surfaces 182a and 182b there is also frictional force, which is proportional to the axial force of the undulating spring 177. Therefore, either friction surface 182a or friction surface 182b, or even both is or are used as the friction surfaces, according to the prevailing conditions.
Instead of using the undulating ring or spring 183 to fix the secondary flywheel mass 103 in position, leaf spring elements can be used for example, which are placed circumferentially between the secondary flywheel mass 103 and the axial piece 145a, and which can then exert pretensioned force in a radial direction. Apart from that it is possible to shape the support plate 146 in the region of its axial piece 145a into an approximately polygonal form. In this way the smallest inner diameter is less than the outer diameter o the secondary flywheel mass 103, so that the flywheel can be frictionally engaged and thus stopped from falling out.
A further possible embodiment of the torque transfer device in accordance with the invention is shown in Figure 4, which has the same or similar components and which uses similar numbers, but which are increased by a further 100.
In contrast to the divided flywheels previously described, the divided flywheel as shown in this instance has the primary flywheel mass 202 designed as a cast part.
Moreover, a hysteresis device 284 is displayed which is positioned between the primary side and the secondary side of the twin mass flywheel, and which causes friction damping. This friction damping may be effective over the whole cf the torsional angle or equally over just part of the torsional angle, in which on the other hand it is possible to design the friction device 284 (which in this case is merely graphically represented) variously in the directions of push and pull.
In order to even out the wear an adjustment device 285 is shown, which amongst other things comprises a sensor spring 286, and which has its function and assembly described for example in the DE-OS 42 39 291, the DE-OS 42 39 239 and the German patent application P 43 22 677.
Particular regard is given to this device and to its contents, which at least in this respect form part of the above application.
The secondary flywheel mass 203 is held with friction engagerent in the pot formed by the axial piece 245a by means cf the undulating spring or undulating ring 283, as has already been described in connection with Figure 3.
There Is an alternative mounting possible, which is similar to that previously described. The disengageable connection 266 - which is positioned between the support plate 246 and the clutch cover 247 -is designed in the same wav as the other configurations given above, and is locked over the open wire ring 279. The wire ring is thus prevented by its angled ends 280 from turning in relation to the support 246.
The sensor spring 286 touches the plate spring 254 with its inner radial region, and in so doing forms the pivot support pad 256 in which the sensor spring tensions the plate spring 254 in its pivot point, which itself points in tne direction of the clutch cover 257. The sensor spring 286 is supported by its outer radial regions on the contact region 288 of support plate 246. With its axial pretensioned force the sensor spring pushes the support plate 246 and the clutch cover 257 away from each other in an axial direction and in such a way that this force is absorbed by the wire ring 279, which is then sealed as a result. In an engaged position, an axial force acting on the contact or friction regions 281 between the support plate 246 and the secondary flywheel mass. This axial force corresponds to the difference between the contact pressure force of plate spring 254 and the tensioned force of sensor spring 286.
Therefore with this arrangement a slip clutch is made, since the following components can be twinned circumferentially with respect to the support plate 246, as they are connected only with friction engagement: the secondary flywheel mass 203, the clutch cover 257 with pressure plate 252, plate spring 254 and sensor spring 286, as well as clutch disc 205. As the sensor spring 286 is likewise connected rotationally secured through recessed sections to the clutch cover 257, one of the friction surfaces of the slip clutch is positioned in the region of the contact area 288 and another friction surface is positioned on the opposite axial side of the cover 257 between this section of the cover 257 and the wire ring 279, which is itself rotationally secured with the support plate 246. The additional friction region 281 between the back pressure plate 203 and the support 246 can however convey the torque, which is proportional to the axial force acting on it. As already explained, the friction regions can also be designed with friction linIngs or coatings.
Figure 5 shows another design possibility of a torque transfer device in accordance with the invention, for which the same or similar parts are used, and for which a similar numbering system is used, although it is increased by a further 100.
The divided flywheel 301 corresponds in its basic assembly to the tin mass flywheel 1 as originally described, but the disengageable connection 366 exhibits a somewhat different construction. While the positioning of wire ring 379 is equivalent to that of the wire ring 79 in Figure 2, the undulating spring 377 is placed between the outer radial piece 387 of clutch cover 364 and the cover plate 346. In this way the clutch cover 364 and the cover plate 346 are both pretensioned directly to each other by means of the undulating spring 377, and they are locked in an axial direction through the wire ring 379. In order to prevent the secondary flywheel mass 303 from falling out of te pot formed by the cover plate 346, retaining tongues l45c are designed in the axIal section 345 of cover plate 346. These retaining tongs 345c are formed by recessed sections built into the cover plate 346, and shaped pointing radially inwards before the secondary flywheel mass 303 is inserted. By means of pushing the secondary flywheel mass 303 into the pot formed by the cover plate 346, these retaining tongues 345c are shaped radially outwards. The tongues then fi and frictionally engage tune secondary flywheel mass 303, so that this connection in turn becomes a component of the slip clutch.
The resilient design of the retaining tongues 345c can on the one hand have an effect on the friction moment of the slip clutch and can, on the other hand, lead to a certain amount of compensation of wear. With the friction clutch 304 in a disengaged position at least three retaining tongues 345c are necessary for the centering and axial retentIon of the secondary flywheel mass 303, although it can be useful to utilise a greater number of retaining tongues 345c.
In the configuration as shown, the cover 364 of the friction clutch 304 is designed as being divided in the region of its radial extension. The outer radial piece 387 of cover 364 is connected radially to the support plate 346 by means of the disengageable connection 366, and has radially inwards radial projections 387b which, viewed circumferentially, are bordered by radial recessed sections 387a. This means that radial projections 387b and radial recessed sections 387a alternate with each other circumferentially.
In the same way, the inner radial pIece 389 of cover 364 contains radial projections 389b in its outer radial region. These projections are bordered by radial recessed sections 389a, so.that here also radial projections 389b and radial recessed sect ions 389a - viewed circurrerentially - alternate with each other. The outer radial piece 387 and the inner radial section 389 of cover 364 are therefore made preferably out of just one plate, so that the radial recessed sections 387a of the outer radial piece 387 of cover 364 are formed, by shaping the projections 389b on the inner radial piece 389 of cover 364 - and vice versa. In other words, this means that the outer radial piece 387 and the inner radial section 389 can be positioned inside one another after their division, similar to the spline shaft in a shaft hub connection, for example.
To form the cover 364 of the friction clutch 304, the outer radial piece 387 and the inner radial section 389 are off-set from each other by "the width o a tooth face" so that the respective radial projections 387b and 389b come to lie on each other. The radial sections 387 and 389 of cover 364, which are thus positioned on top of one another, are joined together in the region of their projections 387b and 389b with the help of connecting screws 390. This screw connection can be separated without destruction for example when repairs are needed due to wear, and can be reassembled after the repairs have been successfully carried out. The screwed-on position or operating state is shown here in Figures Sa and c, while Figure 5b depicts the cover 364 in its disassembled state.
The bearing flange 315 of the twin mass fl;wheel 301 has a collar 315c, which extends radially inwards and forms one of the surfaces facing the combustion engine, at which a dismantling tool (itself able to be inserted from the side remote from the combustion engine) can be used. This type of disrantling tool is supported axially at the collar 315c and enables the plate spring to be pretensioned, thus causing the clutch 30- to be in a disengaged position. This relieves the screw connection for example, which makes it easier to remove the connecting screws 390. Moreover, this type of dismantling tool can help to put the clutch 304 back into a disengaged position, for example in embodiments without a separated cover, so that the clutch disc 305 can be twisted.
Therefore, when there are twin mass flywheels with a slip clutch, as have already been described, it Is possible to relax the sl clutch by tensioning the plate spring 354, and then to twist the components forming the slip clutch opposite the support plate 346 or opposite the primary flywheel mass 302. This has the result that recessed areas, which are designed in the clutch disc and in the plate spring, and which allow the insertion of a screwingup tool, as described for example in Figure 1, can be realigned axially with the heads of the fixing screws so as to connect the twin mass flywheel to the crankshaft of a combustion engine. This collar or frib attachment 315c like the separable cover 364 - is not limited to the embodiment shown in Figure 5, but can also be included in all other embodiments so for example even in the configurations in accordance with the German patent application P 43 20 381. This collar 315c is especially practical in embodiments of twin mass flywheels with a slip clutch, as the recessed areas cr openings for the removal of the crankshaft screws do not have to be aligned after the commissioning of the unit or following the first operation of the slip clutch.
Figure 6 has components which are the same or are similar to those parts already described, and which are numbered in a similar way, although they are increased by a further 100.
The twin mass flywheel 401 shown in Figure 6 has a releasable connection 466 which is designed with a tension ring 491 for easier assembly and dismantling. The positioning of wire ring 479 is unchanged whilst the undulating spring or ring 477 is supported on the cover 464 on one side, and on the other side is supported on the cover plate 446 with the intermediary tension ring 491.
The tension ring 491 is therefore positioned in an axial direction between the undulating sprig 477 and the cover plate 464, as is shown in Figure 6.
In pressure plate 452 there are threaded bores 452a spread out circumferentially, which align with transient bores 465a in the clutch cover 464. Tension screws 491a can be inserted through these transient bores 4=Sa into the threaded bores 452a. Once the screw heads sf the tension screws 491a have been positioned at the clutch cover 464, and when the tension screws 491a are screwed further into the threaded bores 452a, the pressure plate 452 is then moved against the force of the plate spring 454 in an axial direction onto the clutch cover 464, and is thus set in disengagetrent motion. When the pressure plate 452 has been put back a certain distance in an axial direction, a distance which must be greater than that zf the regular clearance, the shoulder 452b which is attached radially outwards on the pressure plate 452 comes to rest on the inner radial region of the tension ring 49. Then, when the axial movement of the pressure plate 452 is continued by the tightening of the tension screws 491, the tension ring 491 is moved in the direction of the clutch cover 464 and thus tensions the undulating spring 47, so that the disengageable connection 466 becomes increasingly relieved. Once the disengageable connection 466 has been completely relieved of all axial force of the undulating spring 477, tne wire ring 479 can be simply removed.
However, it can be sufficient to relieve the disengageable connection 46 of only part of the axial force acting upon it. Figure 6 shows the assembled unit, FIgure 6b shows the tensioning process, and Figure 6c shows the divided unit. Figure 6d shows principally the same assembly, except that here the bores 452a and 465a l-e radially in the region o the plate spring 454, while :n the Figures 6a to c they are positioned outside of the diameter of the plate spring t54.
Further possIble configurations of a torque transfer device in accordance with the invention are shown in Figures 7a and 7b, in which similar numbers are used for the same or similar components, although the numbers are increased by a further 100.
In the ^resigns shown in Figure 7 the cover 564 of the friction clutch 504 engages round the secondary flywheel mass 50 and is coupled to it in the axial region of the secondary flywheel mass 503 by means cf the disengageable connection 566. In the embodiment as given in Figure 7a the secondary flywheel mass 503 is supported on the cover plate 5o6 on the side of the combustion engine, and the cover plate in turn is supported on the cover 564 by the wire ring 579. Therefore the cover 564, the cover plate 546 and the secondary flywheel mass 503 all have radial recessed sections and radial projections, as has already been described, so that they may be assembled together in an axial direction. On the side of the secondary flywheel mass 501 remote from the combustion engine, the secondary flywheel mass is biased by the undulating spring 577 with axial force on the combustion engine. For this, the undulating spring 577 is supported cn one side by the secondary flywheel mass 503, and on the other side by the clutch cover 564. The undulating sprig 577 can, however, be replaced by an equivalent form of the cover plate 546, which itself can then produce spring force in an axial direction by way of tongues which are in equivalent positions and which are shaped axially out of the cover plate surface. In this particular embodiment the secondary flywheel mass 503 is supported on its side remote from the combustion engine directly by the cover 564 of the friction clutch 504, and is pushed against the clutch cover 564 over the spring tongues of the cover 546, which themselves are supported on the cover 564 by the wire <RTI ID=3 564 without trite insertion of the cover plate 546. In this embodiment, the secondary flywheel mass 503 is screwed onto the co-er plate 546 by means of the screws 503a in the outer radial region of the flywheel. The screws are accessible through openings 563 in the prImary flywheel mass 502, which can also help the ventilation.
Figure 8 shows another design possibility of a torque transfer device in accordance with the in-;ention, in the form of a twin mass flywheel. Similar nurrjers have been used for the same or similar components, although the numbers have been increased by a further 100.
The embodiments already described all contain a bearing component, such as in Figure 1 the bearing 6 in the form of a rolling bearing or sliding bearing, which is positioned between the bearing flange 15 and the cover plate 38 (the numbers all refer here to FIgure 1). This component torsionally adjusts and centres the primary and secondary parts of the divided flywheel 1 to one another.
A bearing of this sort is not included in the arrangement as shown in Figure 8, as in this embodiment the primary and secondary parts of the divided flywheel 601 are adjusted to each other directly by the energy accumulators 610. In addItion, the cover plates 638 and 646 - which are substantially adjusted to the contours of the energy accumulators 610 - rest radially outwards on the energy accumulators 610, and are thus supported by the energy accumulators 610. The energy accumulators 610, in turn, are kept centred radially inwards by a guiding shell 692, which may be divided into several parts. This guiding shell 692 serves as a bearing shell and can also act as protection against wear. The guiding shell 692 is fixed on its inner radial by flanges 615 and 530 which are connected =e the first flywheel mass 602. The interior space, which is formed by flanges 615 and 630 and also by cover plates 638 and 646, and in which the energy accumulators 610 and guiding shell 692 are located, is sealed by seals 649 and 650 (which in this instance are represented as components formed in a similar way to plate springs). The space is also at least partly filled with a lubricant. Therefore in the arrangement as shown here, and in addition to their basic function of storing energy, the energy accumulators 610 also assume the role of adjusting and centering in relation to each other the primary flywheel mass 602 and the secondary flywheel mass 603 with the connected friction clutch.
Figure 9 contains parts which are the same as or are similar to those previously described, and which are numbered in a similar fashion, although the numbers are increased by another 100.
The divided flywheel 701 is assembled in a similar fashion to the divided flywheel 601, except that the energy accumulators do not act as the bearding for the primary flywheel mass 702 and secondary flywheel mass 703. In this arrangement the primary and secondary parts of the twin mass flywheel 701 are mounted relative to each other by flange 793 and cover plate 738. Flange 793, which is in one piece at least in its axial direction, replaces the functions of flanges 615 and 630 in Figure 8 for example, and in this instance is produced as a sintered piece.
Slide shoes 794 are positioned between the outer radial region of flange 793 and the adjoining section of cover plate 738 which mainly extends in an axial direction. Not only do these shoes ensure that the parts are exactly centred to one another, but they also reduce the amount of wear Ly means of their sliding properties. These sliding surfaces or slide shoes 794 are mainly fixed to the three or more radial extensions of flange 793 by a positive locking for example, and are preferably made out of a synthetic material such as PE, PA or PEEK (and strengthened by fibres if necessary) In addition to their function of acting as seals, the seas 749 and 750 can be enlisted to prevent any wobbling occurring between the first flywheel mass 702 and the second lywheel mass 703, and in so doing they reinforce the centering function of the slide shoes 749. Also in Figure 9a the seal 750 is designed with a run-up face for the cover plate 738, in order that the cover plate 738 is pressed axially against this run-up face of the seal 750 by the resilient seal 749. In this instance the seal 750 is made as a piece of synthetic material. Figure 9b shcs a two-piece seal 750, containing a machined metal part and a part like a plate spring, which is in turn positioned between the cover plate 738 and the flange 793. The remainder of the assembly corresponds with that already described above in connection with Figure 9a.
The bearing through the energy accumulators 610 and slide shoes 794, as described in connection with Figures 8 and 9, is not limited only to the embodiments sown. It can, for example, also be used in embodiments which are described in connection with the German patent application P 43 20 381.
The invention is not limited merely to the embodiments as shown and as described above. It also encc=casses design variations which can be formed by the combination of individual features.
Reference is also made to the disclosed content of the German patent applications P 43 20 382, P 3 11 908, P 43 15 209, P 43 22 677 as well as the DE-OS 42 39 289 and the DE-OS 42 3 291, to which special attention has been paid here and which form part of the disclosure of the above application.
This applIcation is divided from copending application 9712813.6 which describes and claims three different aspects cf an apparatus for transmitting torque.
The first aspect provides apparatus for transmitting torque, comprising a first flywheel connectable with a rotary output element; a second flywheel rotatable with as well as relative to the first flywheel about a common axis and connectable with a rotary input element; and means for opposing rotation of said flywheels relative to each other including at least one damper having energy storing means which opposes relative rotation between the flywheels, said at least one damper constituting a torque path between said flywheels, wherein the damper has at least one input part and one output part both of which carry abutment regions for the energy storing means, the input part of the damper is connected rotationally fast with the first flywheel, the first flywheel comprises a disc-like component which has an axial projection extending from the radially outer part of the component in the direction of the second flywheel, and a starter gear ring, the second flywheel is at least partly surrounded by the axial profection, and the first flywheel has securing means through which the flywheel tan be secured to a rotary output element, the securing means being located radial 1 inwardly of and radially adjacent to the damper.
The second aspect provides apparatus for transmitting torque, comprising a first flywheel connectable with a rotary output element; a second flywheel rotatable with as well as relative to the first flywheel about a common axis and connectable with a rotary input element; and means for opposing rotation of said flywheels relative to each other including at least one damper hazing energy storing means which opposes relative rotation between the flywheels, said at least one damper constituting a torque path between said flywheels, wherein the first flywheel comprises a disc-like component which has an axial projection extending from the radially outer part of the component in the direction of the second flywheel, a starter gear ring, securing means positioned radially inwardly cf the disclike component or securing the first flywheel to a rotary output element, and openings radially outside the energy storing means for access to fastening means for securing the second flywheel.
The third aspect provides apparatus for transmitting torque, comprising a first flywheel çonnectible with a rotary output element; a second flywheel rotatable with as well as relative to the said first flywheel about a common axis and connectable with a rotary input element; and means for opposing rotation of said flywheels relative to each other including at least one damper having energy storing means which opposes relative rotation between the flywheels, said at least one damper constitutIng a torque path between said flywheels, wherein the apparatus has, considered in a radial direction from inwards outwards, the following features: - a bearing between the two flywheels, - securing means for mounting the apparatus on a rotary output element - the energy storing means of the damper - a component of the second flywheel which has a friction surface for a clutch disc.
Application 9712813.6 is itself divided from copending application 9412227.2 which describes end claims three different aspects of an apparatus for transmitting torque.
The first aspect provides apparatus cornrising: a first flywheel connectable with a rotary output element; an engageable and disengageable friction clutch connectable with a rotary input element; a second flywheel rotatable with as weal as relative to said first flywheel about a common axis; and means for opposing rotation of said flywheels relative to each other including at least one damper having energy storing means acting in a circumferential direction of said flywheels, said at least one damper and said friction clutch constituting a power train between said first flywheel and the input element, said power train including a slip clutch having means for separably zoupling a first and a second component of the power train to each other and means. for limiting the magnitude of torque transmittable between said first flywheel and the input element in the engaged condition of said frIction clutch.
The second aspect provides apparatus for transmitting torque comprising a first flywheel connectable to a rotary output element and a power train, said power train comprising: an engageable and disengageable friction clutch connectable to an input element; a second flywheel rotatable ith as well as relative to said first flywheel about a cor.non axis; means for opposing rotation of said flywheels relative to each other includIng at least one damper having energy storing means, an input member between said first flywheel and said energy storing means, and an output member disposed between said energy storing means and said second flywheel and including an enclosure at least partially confining said energy storing means; means for limiting the magnitude of torque transmittable between said first flywheel and the input elerent in the engaged condition of said friction clutch; and means for separably connecting a first and a second component of said power train to each other, said components forming part of a slip clutch.
The third aspect provides apparatus for transmitting torque between rotary input and output elements, comprising a first flywheel connectable to the output element and a power train between said first flywheel and the input element, said power train comprising: an engageable and disengageable friction clutch including a second flywheel rotatable with as well as relative to said first flywheel about a common axis; means for opposing rotation of said flywheels relative to each other, including at least one damper having energy string means acting in a circumferential direction of said flywheels; means for separably connecting a first component to a second component of said power train, said first and second components forming part of a slip clutch; and means for limiting the magnitude of torque which is being transmitted between said first flywheel and the input element.

Claims (19)

1. Apparatus for transmitting torque, comprising a first flywheel mass connectable with a rotary output element; a second flywheel mass rotatable with as well as relative to the first flywheel mass about a colon axis and connectable with a rotary input element; and means for opposing rotation of said flywheel masses relative to each other including at least one damper having energy storing means acting in a circumferential direction of said flywheel masses, said at least one damper constituting a torque path between said flywheel masses wherein the first flywheel mass comprises a disc-like component which has an axial projection extending from the radially outer part of the component in the direction of the second flywheel mass, and a starter gear ring, and has radially inwardly positioned securing means for securing the flywheel mass to a rotary output element and the disc-like component has openings radIally outside the energy storing means for fastening the second flywheel mass by means of fastenings which are accessible through the openings.
2. Apparatus as claimed in Claim 1, wherein the first flywheel mass is a sheet metal part.
3. Apparatus as claimed in Claim 1 or Claim 2, wherein the securing means are openings for receiving threaded fasteners.
4. Apparatus as claimed in any preceding claim, wherein the fastenings for the second flywheel mass are accessible from the side of the first flywheel mass facing away from the second flwheel mass through the openings and into the second flywheel mass.
5. Apparatus for transmitting torque comprising a first flywheel mass connectable with a drive and a second flywheel mass connectable with the first fly^:^eel mass through a torsion vibration damper, the second flywheel mass being rotatable relative to the first fly;.ieel mass and the clutch housing of a friction clutch beIng fitted on the second flywheel mass, the friction clutch having a rotationally fixed but axially displaceable pressure plate, an energy storing means, such as a diaphragm spring, biasing the pressure plate and a clutch disc arranged between tne pressure plate and a counter pressure plate, wherein at least the counter pressure plate (which forms a component of the second flywheel mass), the clutch disc, the pressure plate, the clutch housing and the energy storing means form a preassembled unit which is connectable as such by means of fasteners with a component provided on the first flywheel mass, wherein the first flywheel mass has openings through which the fastenings can be tightened from the side of the first flywheel mass facing away from the second flywheel mass.
6. Apparatus as claimed in any preceding clay, wherein the second flywheel mass is connectable trough an engageable and disengageable friction clutch with a rotary input element.
7. Apparatus as claimed in any preceding clay, wherein between the two flywheel masses, at least one hysteresis device is provided which is arranged radially outside the longitudinal axis of the energy storing means of the damper which acts between the two flywheel masses.
8. Apparatus as claimed in any preceding claims, wherein the axial projection of the first flywheel mass is formed by an annular inertia ring which is fastened at the radially outer region of the flange like c07onent.
9. Apparatus as claimed in Claim 8, wherein the inertia ring is made as a folded plate.
10. Apparatus as claimed in Claim 8 or Clair. 9, wherein the inertia ring, considered in cross-section Ls angularly formed.
11. Apparatus as claimed in any one of ClaIms 8 to 10, wherein the inertia ring carries the starter ring gear.
12. Apparatus as claimed in any preceding claim, wherein the damper has an input part, rotationally connected with the first flywheel mass, as well as an output part rotationally connected with the second fly heel mass, wherein the rotational connection between the damper input part and the first flywheel mass lies radially inside the energy storing means of the damper, and the connection between the output part of the second flywheel is provided radially outside the energy storing means.
13. Apparatus as claimed in any preceding claim, wherein the two flywheel masses as well as the friction clutch carried by the second flywheel mass form one constructional nit.
14. Apparatus as claimed in any preceding claim, wherein fastening means for connecting the first flywheel mass with the rotary output element are integrated in the Apparatus and are secured against loss.
15. Apparatus as claimed in any preceding claim, wherein a component of the damper which is biased by the energy storage means serves as a bearing between the two flywheel masses.
16. Apparatus as claimed in Claim 15, characterised in that the component has openings for receiving fastenings.
17. Apparatus as claimed in any preceding claim, wherein the friction clutch carried by the second flywheel mass has a diaphragm spring with radially inwardly directed tongues, and in the region of the tongues and/or in the region between the tongues, openings are provided for tightening of fasteners.
18. Apparatus as claimed in any preceding claim, wherein openings for tightening of fastenings are provided in a component of the clutch disc.
Amendments to the claims have been filed as follows CLAIMS 1. Apparatus for transmitting torque, comprising a first flywheel mass connectable with a rotary output element; a second flywheel mass rotatable with as well as relative to the first flywheel mass about a common axis and connectable with a rotary input element; and means for opposing rotation of said flywheel masses relative to each other including at least one damper having energy storing means acting in a circumferential direction of said flywheel masses, said at least one damper constituting a torque path between said flywheel masses wherein the first flywheel mass comprises a disc-like component which has an axial projection extending from the radially outer part of the component in the direction of the second flywheel mass, and a starter gear ring, and has securing means positioned radially inwardly of the energy storing means for securing the first flywheel mass to a rotary output element and the disc-like component has openings radially outside the energy storing means for fastening the second flywheel mass to a component carried by the first flywheel mass by means of fastenings which are accessible through the openings.
2. Apparatus as claimed in Claim 1, wherein the first flywheel mass is a sheet metal part.
3. Apparatus as claimed in Claim 1 or Claim 2, wherein the securing means are openings for receiving threaded fastenings.
4. Apparatus as claimed in any preceding claim, wherein the fastenings for the second flywheel mass are accessible from the side of the first flywheel mass facing away from the second flywheel mass through the openings and into the second flywheel mass.
5. Apparatus for transmitting torque comprising a first flywheel mass connectable with a drive and a second flywheel mass connectable with the first flywheel mass through a torsion vibration damper, the second flywheel mass being rotatable relative to the first flywheel mass and the clutch housing of a friction clutch being fitted on the second flywheel mass, the friction clutch having an axially displaceable pressure plate, an energy storing means biasing the pressure plate and a clutch disc arranged between the pressure plate and a counter pressure plate, wherein at least the counter pressure plate (which forms a component of the second flywheel mass), the clutch disc, the pressure plate, the clutch housing and the energy storing means form a preassembled unit which is connectable as such by means of fastenings with a component carried by the first flywheel mass, wherein the first flywheel mass has openings through which the fastenings can be tightened from the side of the first flywheel mass facing away from the second flywheel mass.
6. Apparatus as claimed in Claim 5, wherein the energy storing means is a diaphragm spring.
7. Apparatus as claimed in any preceding claim, wherein the second flywheel mass is connectable through an engageable and disengageable friction clutch with a rotary input element.
8. Apparatus as claimed in any preceding claim, wherein between the two flywheel masses, at least one hysteresis device is provided which is arranged radially outside the longitudinal axis of the energy storing means of the damper which acts between the two flywheel masses.
9. Apparatus as claimed in any preceding claim, wherein an axial projection of the first flywheel mass is formed by an annular inertia ring which is fastened at the radially outer region of the disc-like component.
10. Apparatus as claimed in Claim 9, wherein the inertia ring is made as a folded plate.
11. Apparatus as claimed in Claim 9 or Claim 10, wherein the inertia ring, considered in cross-section is angularly formed.
12. Apparatus as claimed in any one of Claims 9 to 11, wherein the inertia ring carries the starter ring gear.
13. Apparatus as claimed in any preceding claim, wherein the damper has an input part, rotationally connected with the first flywheel mass, as well as an output part rotationally connected with the second flywheel mass, wherein the rotational connection between the damper input part and the first flywheel mass lies radially inside the energy storing means of the damper, and the connection between the output part of the second flywheel is provided radially outside the energy storing means.
14. Apparatus as claimed in any preceding claim, wherein the two flywheel masses as well as the friction clutch carried by the second flywheel mass form one constructional unit.
15. Apparatus as claimed in any preceding claim, wherein fastening means for connecting the first flywheel mass with the rotary output element are integrated in the apparatus and are secured against loss.
16. Apparatus as claimed in any preceding claim, wherein a component of the damper which is biased by the energy storage means serves as a bearing between the two flywheel masses.
17. Apparatus as claimed in Claim 16, wherein the component has openings for receiving fastenings.
18. Apparatus as claimed in any preceding claim, wherein the friction clutch carried by the second flywheel mass has a diaphragm spring with radially inwardly directed tongues, and in the region of the tongues and/or in the region between the tongues, openings are provided for tightening of fasteners.
19. Apparatus as claimed in any preceding claim, wherein openings for tightening of fastenings are provided in a component of the clutch disc.
GB9722621A 1993-06-19 1994-06-17 Torque transfer apparatus Expired - Fee Related GB2315316B (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE4320381 1993-06-19
DE4333460 1993-09-30
GB9712813A GB2312945B (en) 1993-06-19 1994-06-17 Torque transfer device

Publications (3)

Publication Number Publication Date
GB9722621D0 GB9722621D0 (en) 1997-12-24
GB2315316A true GB2315316A (en) 1998-01-28
GB2315316B GB2315316B (en) 1998-04-08

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Application Number Title Priority Date Filing Date
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GB (1) GB2315316B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1862687A3 (en) * 2006-06-01 2010-09-29 ZF Friedrichshafen AG Torque transmission assembly for the power transmission of a vehicle drive train
EP3109497A1 (en) * 2015-06-26 2016-12-28 Schaeffler Technologies GmbH & Co. KG Torsional vibration damper with adjusting device
WO2020083433A1 (en) * 2018-10-23 2020-04-30 Schaeffler Technologies AG & Co. KG Clutch unit having a cardan spring for forming an axially resilient connection between a driving ring and a clutch cover

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2184518A (en) * 1985-12-19 1987-06-24 Luk Lamellen & Kupplungsbau Arrangement for compensating for rotary shocks
GB2273334A (en) * 1992-12-10 1994-06-15 Fichtel & Sachs Ag Dual-mass flywheel
GB2277791A (en) * 1993-05-07 1994-11-09 Luk Lamellen & Kupplungsbau Flywheel and torsional vibration damper

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2184518A (en) * 1985-12-19 1987-06-24 Luk Lamellen & Kupplungsbau Arrangement for compensating for rotary shocks
GB2273334A (en) * 1992-12-10 1994-06-15 Fichtel & Sachs Ag Dual-mass flywheel
GB2277791A (en) * 1993-05-07 1994-11-09 Luk Lamellen & Kupplungsbau Flywheel and torsional vibration damper

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1862687A3 (en) * 2006-06-01 2010-09-29 ZF Friedrichshafen AG Torque transmission assembly for the power transmission of a vehicle drive train
EP3109497A1 (en) * 2015-06-26 2016-12-28 Schaeffler Technologies GmbH & Co. KG Torsional vibration damper with adjusting device
WO2020083433A1 (en) * 2018-10-23 2020-04-30 Schaeffler Technologies AG & Co. KG Clutch unit having a cardan spring for forming an axially resilient connection between a driving ring and a clutch cover

Also Published As

Publication number Publication date
GB2315316B (en) 1998-04-08
GB9722621D0 (en) 1997-12-24

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