GB2346949A - Flywheel assembly - Google Patents
Flywheel assembly Download PDFInfo
- Publication number
- GB2346949A GB2346949A GB0007582A GB0007582A GB2346949A GB 2346949 A GB2346949 A GB 2346949A GB 0007582 A GB0007582 A GB 0007582A GB 0007582 A GB0007582 A GB 0007582A GB 2346949 A GB2346949 A GB 2346949A
- Authority
- GB
- United Kingdom
- Prior art keywords
- axial
- flywheel
- chamber
- bearing
- journal bearing
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/10—Suppression of vibrations in rotating systems by making use of members moving with the system
- F16F15/12—Suppression 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
- F16F15/131—Suppression 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
- F16F15/13164—Suppression 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
- F16F15/13171—Bearing arrangements
- F16F15/13178—Bearing arrangements comprising slide bearings
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Mechanical Operated Clutches (AREA)
Abstract
A flywheel assembly comprises input and output-side flywheels 1, 26 rotatable relative to one another against the action of a torsional damping device 8. The output-side flywheel remote from an I/C engine crankshaft 23 is guided by a bearing assembly radially 14 and axially 21 with respect to the input-side flywheel. The dial journal bearing 21 forms a boundary for a chamber 6 containing viscous medium and at least partially receiving the torsional damping device 8. One axial side of the axial bearing engages axially with one of the flywheels to form a seal 70 for the chamber, and the other axial side of the bearing has an axial projection 60 which is radially outwards of and in axial overlap with, a component 64 forming part of the other flywheel. This arrangement forms a seal 35 for the chamber which virtually eliminates loss of viscous medium.
Description
FLYWHEEL ASSEMBLY
The invention relates to a flywheel assembly of the kind comprising input-side and output-side flywheels, relatively rotatable against the action of a torsional damping device, the output-side flywheel being guided radially and axially with respect to the input-side flywheel through a bearing assembly, the bearing assembly having at least one axial journal bearing forming part of a boundary of a chamber containing viscous medium and at least part of the torsional damping device.
DE 44 17 108 Al shows a flywheel assembly of the kind set forth, in which the input-side flywheel is connected to an input drive, such as for example the crankshaft of an internal combustion engine. The outputside flywheel is connected to a friction clutch. The bearing assembly is formed by a journal bearing which is made in two parts with a radially inner ring connected to the input-side flywheel and a radially outer ring connected to the output-side flywheel. Each ring has a radially extending limb, and the bearing assembly acts as an axial journal bearing. The radial limb of the radially inner ring forms the boundary of the chamber which receives the torsional damping device.
With such an axial journal bearing, when the clutch is engaged and the axial force of its actuating spring and/or the axially acting pre-load of a clutch withdrawal mechanism is effective, the output-side flywheel is urged towards the input-side flywheel so that the radial limbs of the two rings are held in engagement. This provides a seal for the chamber in the region of the bearing assembly.
During transport or assembly of the flywheel assembly or on measuring it no axial pre-load is applied and a gap can arise between the radial limbs of the two rings. This can also happen, albeit briefly, even with an axial pre-load with the clutch withdrawn, when swashplate-like wobbling or tumbling movements can cause the output-side flywheel to lift away. In these circumstances viscous medium in the chamber escapes from the flywheel assembly through the bearing assembly. A reduced amount of viscous medium adversely affects operation of the flywheel assembly, as it reduces the damping behaviour of the torsional damping device.
The invention is based on solving the problem of constructing a flywheel assembly of the kind set forth in the region of an axial journal bearing in such a way that the escape of viscous medium from the chamber at the journal bearing is substantially prevented.
According to the present invention, in a flywheel assembly of the kind set forth one axial side of the axial journal bearing engages axially with one of the flywheels to form a seal for the chamber and the other axial side of the axial journal bearing has an axial projection which is radially outwards of, and in axial overlap with, a component forming part of the other flywheel.
This provides a particularly simple construction. The axial projection of the axial journal bearing, because it is radially outwards of and in axial overlap with the adjacent component of the input-side flywheel, forms an impact surface for viscous medium which reaches the region of the axial journal bearing as a spray. Since this spray largely loses its kinetic energy on impact with the axial projection, it has insufficient energy for it to leave the chamber. Preferably, a face on the other axial side of the axial journal bearing engages the component to form a seal. This improves the sealing further.
Advantageously, each axial side of the axial journal bearing has a radial sealing face engaging the respective flywheel, the sealing faces together with the axial projection forming the seal for the chamber.
An embodiment of the invention is illustrated by way of example in the accompanying drawings, in which:
Figure 1 shows a longitudinal section through half of a flywheel
assembly falling outside the scope of the invention,
with an axial journal bearing with a seal associated with its
peripheral region;
Figure 2 is an enlarged detail of the circled region in Figure 1 to
illustrate the seal; and
Figure 3 is similar to Figure 2, but with a journal bearing in
accordance with the invention.
The flywheel assembly shown in Figure 1 is for mounting in the drive train of a motor vehicle (not shown) between a crankshaft 23 of an internal combustion engine (not shown) as an input drive 22, and a friction clutch (not shown). The assembly of Figures 1 and 2 falls outside the scope of the claims.
The flywheel assembly comprises an input-side flywheel 1 and an output-side flywheel 26 with a torsional damping device 8 between them.
The input-side flywheel 1 has a radially outwardly extending primary flange 2 with a peripheral axial rim 3 on which there is mounted a starter ring 4 meshing with a starter pinion (not shown). A sealing plate 5 is secured to the axial rim 3. The sealing plate 5 projects radially inwards and has on its radially inner end a plate spring acting as an axial energy storing device 57. The sealing plate 5, with the axial rim 3 and the primary flange 2 define a chamber 6 for viscous medium in the radially outer region of which there are arranged circumferentially extending resilient elements 7 of the damping device 8. The resilient elements 7 are acted on at one end by locating elements 9 on the primary flange 2, whilst at the other end they abut against radially outwardly projecting fingers 10 on a hub disc 12 connected by rivets 25 to the output-side flywheel 26.
The hub disc 12 thus effectively forms part of the flywheel 26.
The hub disc 12 is rigidly connected to an annulus 11 of planetary gearing and has on its radially inner end a secondary hub 13 for receiving a radial journal bearing 20 of a bearing assembly 14. The radial journal bearing carries in its turn a primary hub 15 for the primary flange 2.
Looking axially, the primary hub 15 extends from the primary flange 2, with its free end towards the hub disc 12, whilst the secondary hub 13 extends from the hub disc 12 with its free end towards the primary flange 2.
The radial journal bearing 20 mounts the hub disc 12 and with it the output-side flywheel 26 rotatably on the input-side flywheel 1.
Radially immediately outside the radial journal bearing 20 the hub disc 12 is provided with assembly openings 17 through which attachment means 18 indicated only by broken lines in Figure 1, are inserted. The flywheel is mounted by the attachment means 18 on the crankshaft 23, the crankshaft 23 having a stub shaft 62 projecting into the primary hub 15 of the input-side flywheel 1 into a radial locating socket 28 in the input-side flywheel 1.
An axial journal bearing 21 of the bearing assembly 14 is mounted radially outwards of the attachment means 18, between the hub disc 12 and a ring 19 held by the attachment means 18 in engagement against the primary flange 2. The ring 19 effectively forms part of the input-side flywheel 1 and has an axial projection 32 in its radially outer peripheral region extending towards the hub disc 12. The projection 32 is radially outside the axial bearing 21, and extends along a substantial part of its axial extent (see Figure 2). The hub disc 12 has a further axial projection 34, radially aligned with the axial projection 32.
This axial projection 34 projects towards the axial projection 32 with a clearance gap 36 formed between them. The projection 34 projects proud of a recess 33 which is formed in the hub disc 12 on its side adjacent the ring 19. The axial journal bearing 21 is received in the recess 33 and engages the side of the ring 19 adjacent the hub disc 12 radially inwards of its axial projection 32. A chamber 37 is defined radially between the periphery of the axial journal bearing 21 and the axial projections 32 and 34. The axial journal bearing 21 acts, together with the clearance gap 36 between the axial projections 32 and 34, as a seal 35 for the chamber 6 during operation of the assembly. The axial journal bearing 21 has on its side adjacent the input-side flywheel 1 an engaging face 55 for this flywheel and on its opposing side and engaging face 56 for the output-side flywheel 26. The two flywheels 1, 26 are urged towards one another by the axial energy-storing device 57 and against the respective associated engaging faces 55,56 of the axial journal bearing 21.
The primary flange 2 has bearing extensions projecting towards the hub disc 12. On each bearing extension is rotatably mounted a planet wheel 50, which forms part of the planetary gearing and has a toothed engagement with the annulus 11.
When the flywheel assembly is rotating, viscous medium is urged radially outwards by centrifugal force, away from the bearing 21.
However when the assembly is stationary, viscous medium in the chamber 6 can drip from the above-mentioned planet wheel 50 under gravity onto the axial projection 32 of the ring 19. The axial projection 32 has a slight inclination towards the primary flange 2, so that this dripping viscous medium is diverted towards the primary flange 2 and a radially larger ring 38 provided on the planet wheel 50. Viscous medium which reaches the ring 38 is thrown radially outwards by centrifugal force on subsequent operation of the assembly. Only that portion of viscous medium which drips axially between the planet wheel 50 and the hub disc 12 can reach the clearance gap 36 between the two axial projections 32 and 34. This is usually a very small amount. With the flywheel stationary the medium may be able to pass through the clearance gap 36 into the chamber 37.
However, viscous medium in the chamber 37 dripping radially on the periphery of the axial journal bearing 21 cannot go any further between the ring 19 and the axial journal bearing 21, or between the bearing 21 and the hub disc 12 in a radially inward direction, because of the engagement of the bearing 21 against the ring 19 and the hub disc 12 by the spring 57. It cannot therefore escape through the assembly openings 17. On the contrary, as soon as the flywheel assembly rotates again on subsequent use, viscous medium in the chamber 37 is thrown back radially through the gap 36 and back into the chamber 6. Escape of viscous medium from the chamber 6 under normal circumstances is as good as eliminated. The spring 57 also ensures engagement of the bearing 29 and the flywheels on wobbling movement of the flywheel 26.
Figure 3 shows an embodiment of the axial journal bearing 21 illustrating the invention, and corresponding reference numerals have been applied to corresponding parts. In Figure 3 the bearing 21 has an axial projection 60 in its radially outer region extending towards the ring 19 which acts as a component 64 fixed to the input-side flywheel 1. The axial projection 60 is radially outwards of, and in axial overlap with the ring 19, so that its end is enclosed by the projection 60. Radially inwards of this axial projection 60 the axial journal bearing 21 has on its side 61 adjacent the ring 19, a radial engaging face 66 for the ring 19. As before, the axial journal bearing 21 has its other axial side 68 abutting against the output-side flywheel 26. A first sealing face 70 is formed between the output-side flywheel 26 and the side 68 of the axial journal bearing 21, and a second sealing face 72 is formed on its other side 61 in the region of the engaging face 66 for the ring 19, so that the escape of viscous medium from the chamber 6 is successfully prevented. The sealing faces 70 and 72 act together with the axial projection 60 to form a seal 35 for the chamber 6.
In operation, the axial projection 60 forms an impact surface for viscous medium passing axially between the teeth as the planet wheels 50 roll on the annulus 11 and accelerated towards the bearing 21 as a spray.
As the spray largely loses its kinetic energy on impact with the axial projection 60, it has insufficient energy to leave the chamber 6, between the sealing faces 70,72 and the flywheels.
Claims (4)
- CLAIMS 1. A flywheel assembly of the kind set forth, in which one axial side of the axial journal bearing engages axially with one of the flywheels to form a seal for the chamber and the other axial side of the axial journal bearing has an axial projection which is radially outwards of, and in axial overlap with, a component forming part of the other flywheel.
- 2. A flywheel assembly as claimed in claim 1, in which a face on the other axial side of the axial journal bearing engages the component to form a seal.
- 3. A flywheel assembly as claimed in claim 2, in which each axial side of the axial journal bearing has a radial sealing face engaging the respective flywheel, the sealing faces together with the axial projection forming the seal for the chamber.
- 4. A flywheel assembly of the kind set forth substantially as illustrated herein with reference to and as illustrated in Figure 3 of the accompanying drawings.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19639562 | 1996-09-26 | ||
DE19726262A DE19726262C2 (en) | 1996-09-26 | 1997-06-20 | Flywheel mass device with an axial plain bearing as a seal |
GB9720412A GB2319322B (en) | 1996-09-26 | 1997-09-26 | Flywheel assembly |
Publications (3)
Publication Number | Publication Date |
---|---|
GB0007582D0 GB0007582D0 (en) | 2000-05-17 |
GB2346949A true GB2346949A (en) | 2000-08-23 |
GB2346949B GB2346949B (en) | 2001-03-07 |
Family
ID=27216685
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0007582A Expired - Fee Related GB2346949B (en) | 1996-09-26 | 1997-09-26 | Flywheel assembly |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2346949B (en) |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4962838A (en) * | 1989-09-29 | 1990-10-16 | Eaton Corporation | Viscous damper with low seal drag torque |
US4963119A (en) * | 1989-02-03 | 1990-10-16 | Valeo | Torsion damping device including viscous damping means, in particular for automotive vehicles |
EP0403338A1 (en) * | 1989-06-12 | 1990-12-19 | Valeo | Torsional vibration damper with circumferentially arranged elastic means in a leak-proof casing, especially for motor vehicles |
WO1995014181A1 (en) * | 1993-11-15 | 1995-05-26 | Valeo | Flywheel, in particular for motor vehicles |
GB2310910A (en) * | 1996-03-08 | 1997-09-10 | Fichtel & Sachs Ag | Flywheel assembly |
GB2310912A (en) * | 1996-03-08 | 1997-09-10 | Fichtel & Sachs Ag | Flywheel having masses projecting radially beyond teeth of pl anet wheel. |
GB2328266A (en) * | 1997-06-30 | 1999-02-17 | Mannesmann Sachs Ag | Torsion vibration damper with planetary gearing |
-
1997
- 1997-09-26 GB GB0007582A patent/GB2346949B/en not_active Expired - Fee Related
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4963119A (en) * | 1989-02-03 | 1990-10-16 | Valeo | Torsion damping device including viscous damping means, in particular for automotive vehicles |
EP0403338A1 (en) * | 1989-06-12 | 1990-12-19 | Valeo | Torsional vibration damper with circumferentially arranged elastic means in a leak-proof casing, especially for motor vehicles |
US4962838A (en) * | 1989-09-29 | 1990-10-16 | Eaton Corporation | Viscous damper with low seal drag torque |
WO1995014181A1 (en) * | 1993-11-15 | 1995-05-26 | Valeo | Flywheel, in particular for motor vehicles |
GB2310910A (en) * | 1996-03-08 | 1997-09-10 | Fichtel & Sachs Ag | Flywheel assembly |
GB2310912A (en) * | 1996-03-08 | 1997-09-10 | Fichtel & Sachs Ag | Flywheel having masses projecting radially beyond teeth of pl anet wheel. |
GB2328266A (en) * | 1997-06-30 | 1999-02-17 | Mannesmann Sachs Ag | Torsion vibration damper with planetary gearing |
Also Published As
Publication number | Publication date |
---|---|
GB0007582D0 (en) | 2000-05-17 |
GB2346949B (en) | 2001-03-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20050926 |