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Sommaire du brevet 2044094 

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L'apparition de différences dans le texte et l'image des Revendications et de l'Abrégé dépend du moment auquel le document est publié. Les textes des Revendications et de l'Abrégé sont affichés :

  • lorsque la demande peut être examinée par le public;
  • lorsque le brevet est émis (délivrance).
(12) Brevet: (11) CA 2044094
(54) Titre français: ACCOUPLEMENT SOUPLE PAR TORSION
(54) Titre anglais: FLEXIBLE TORSION COUPLING
Statut: Périmé et au-delà du délai pour l’annulation
Données bibliographiques
(51) Classification internationale des brevets (CIB):
  • F16D 3/76 (2006.01)
  • F16D 3/50 (2006.01)
  • F16D 3/74 (2006.01)
(72) Inventeurs :
  • ANDRA, RAINER-HORST (Allemagne)
  • EICHHORN, JURGEN (Allemagne)
(73) Titulaires :
  • CARL FREUDENBERG
(71) Demandeurs :
  • CARL FREUDENBERG (Allemagne)
(74) Agent: BORDEN LADNER GERVAIS LLP
(74) Co-agent:
(45) Délivré: 1995-01-17
(22) Date de dépôt: 1991-06-07
(41) Mise à la disponibilité du public: 1991-12-10
Requête d'examen: 1991-06-07
Licence disponible: S.O.
Cédé au domaine public: S.O.
(25) Langue des documents déposés: Anglais

Traité de coopération en matière de brevets (PCT): Non

(30) Données de priorité de la demande:
Numéro de la demande Pays / territoire Date
P 40 18 596.6 (Allemagne) 1990-06-09

Abrégés

Abrégé anglais


A flexible torsion coupling for two machine elements is
disclosed. The coupling includes a pair of rings which are
respectively provided on the machine elements and partially surround
each other at a radial distance. A first ring of the pair of rings
has an axially open, U-shaped profile and defines a space that is at
least partly divided by the second ring of the rings into a pair of
chambers, which surround each other in radial direction. A radial
bearing is provided in one of the chambers and a damping element is
provided in the other chamber. The torsion coupling has a smaller
axial length and permits, for example, the transmission of rotational
forces of a shaft to a pulley connected with the shaft by the torsion
coupling.

Revendications

Note : Les revendications sont présentées dans la langue officielle dans laquelle elles ont été soumises.


THE EMBODIMENTS OF THE INVENTION IN WHICH AN EXCLUSIVE
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A flexible portion coupling for a pair of machine elements and having an axis of
rotation, comprising first and second mutually surrounding, radially spaced apart rings
respectively attachable to the machine elements and defining an intermediate gap, a
damping element and a radial bearing positioned in the intermediate gap for relatively
rotatably connecting the first and second rings, the first ring having a U-shaped cross-
section and defining an annular space, the annular space being opened in axial direction
of the coupling and being divided by the second ring into a first pair of inner and outer
chambers which at least partly surround one another in radial direction, and the radial
bearing being positioned in one of the first inner and outer chambers and a dampening
element being positioned in the other of the first inner and outer chambers.
2. A coupling as defined in Claim 1, wherein the damping element connects a pair of
radially opposite, spaced apart surfaces of the first and second rings.
3. A coupling as defined in Claim 1, wherein the damping element connects a pair of
radially opposite, spaced apart surfaces of the first and second rings.
4. A coupling as defined in Claim 3, wherein the damping element and the radial
bearing are positioned in a common radial plane.
5. A coupling as defined in Claim 1, 2, 3 or 4, wherein the radial bearing is a slide
bearing.

6. A coupling as defined in Claim 1, 2, 3 or 4, wherein the radial bearing is a
deep-groove ball bearing.
7. A coupling as defined in Claim 1, 2, 3 or 4, wherein the second ring has an
annular projection that is radially spaced apart from and surrounds that leg of the
U-shaped profile of the first ring which radially outwardly surrounds the second ring,
wherein the annular gap resulting from the radial spacing of the annular protrusion and
the second ring is at least partly divided by a third ring into a pair of second chambers,
which at least partially surround each other in radial direction, and wherein a second
radial bearing is provided in one of the second chambers and a second damping element
is provided in the other of the second chambers for relatively rotatably and elastically
supporting the third ring.
8. A coupling as defined in Claim 5, wherein the second ring has an annular
projection that is radially spaced apart from and surrounds that leg of the U-shaped
profile of the first ring which radially outwardly surrounds the second ring, wherein the
annular gap resulting from the radial spacing of the annular protrusion and the second
ring is at least partly divided by a third ring into a pair of second chambers, which at
least partially surround each other in radial direction, and wherein a second radial
bearing is provided in one of the second chambers and a second damping element is
provided in the other of the second chambers for relatively rotatably and elastically
supporting the third ring.
9. A coupling as defined in Claim 6, wherein the second ring has an annular
projection that is radially spaced apart from and surrounds that leg of the U-shaped
profile of the first ring which radially outwardly surrounds the second ring, wherein the

radial gap resulting from the radial spacing of the annular protrusion and the second
ring is at least partly divided by a third ring into a pair of second chambers, which at
least partially surround each other in radial direction, and wherein a second radial
bearing is provided in one of the second chambers and a second damping element is
provided in the other of the second chambers for relatively rotatably and elastically
supporting the third ring.
10. A flexible portion coupling for a pair of machine elements and having an axis of
rotation, comprising first and second mutually surrounding, radially spaced apart rings
respectively attachable to the machine elements and defining an intermediate gap, a
damping element and a radial bearing positioned in the intermediate gap for relatively
rotatably connecting the first and second rings, the first ring having a U-shaped cross-
section and an inertia ring affixed to one of the first and second rings by an
intermediate damping layer made of rubbery material, and defining an annular space, the
annular space being opened in axial direction of the coupling and being divided by the
second ring into a first pair of inner and outer chambers which at least partly surround
one another in radial direction, and the radial bearing being positioned in one of the first
inner and outer chambers and a dampening element being positioned in the other of the
first inner and outer chambers.
11. A coupling as defined in claim 10, wherein the damping layer connects a contact
surface of the inertia ring with a radially opposite contact surface of the one of the first
and second rings associated with the inertia ring.
12. A coupling as defined in claim 11, wherein the inertia ring in cross-section has
an axial leg which extends parallel to the axis of the coupling, the contact surface of the

inertia ring being a surface of the leg.
13. A coupling as defined in claim 10 or 11, wherein the inertia ring in cross-section
has an axial leg which extends parallel to the axis of the coupling, and the other of the
first and second rings is spaced apart from and in radial direction surrounds the axial leg
of the inertia ring.
14. A coupling as defined in claim 12, wherein the inertia ring in cross-section has
an axial leg which extends parallel to the axis of the coupling, and the other of the first
and second rings is spaced apart from and in radial direction surrounds the axial leg of
the inertia ring.

Description

Note : Les descriptions sont présentées dans la langue officielle dans laquelle elles ont été soumises.


20140!3~
FLEXIBLE TORSION COUPLING
The invention relates to a flexible torsion coupling for two
machine elements, wherein a pair of rings are respectively provided on
the machine elements, which rings surround each other at a radial
spacing and wherein a damping element of rubber and a radial bearing
are positioned in the gap resulting from the radial spacing to connect
the rings parallel to each other. Particularly, the invention relates
to a flexible torsion coupling for use in, for example, torsion
dampers of internal combustion engines.
Such a coupling is used in the torsion damper disclosed in German
Utility Model 89 12 387.5. The damping element and the radial bearing
are therein positioned side by side in axial direction. This
construction creates a coupling of a relatively large axial length.
It is an aspect of the invention to provide an improved flexible
torsion coupling of a shorter axial length.
Accordingly, the invention provides a flexible torsion coupling
for two machine elements. The coupling includes a pair of first and
second rings, which rings are respectively connected to the two
machine elements and radially spaced apart surround each other. A
damping element and a radial bearing are positioned in the radial gap
created by the radial spacing of the rings. The first ring has an
axially open, U-shaped cross-section and the space defined by the
U-shaped first ring is at least partly divided by a second ring into a
pair of first chambers, which at least partly surround each other in
radial direction. The radial bearing is positioned in one of the
first chambers and the damping element is positioned in the other of
the first chambers. The damping element and the radial bearing may be
positioned to overlap in an axial direction, which provides for a
relatively shorter axial length of a torsion coupling in accordance
with the invention.

- 204~094
Nonetheless, a good supporting of the rings on each other is
guaranteed, which allows the transmission of radial forces and renders
the use of such a torsion coupling in connection with pulleys and
torsion dampers more suitable.
The damping element may connect two axially spaced apart opposing
surfaces of the two rings, which permits the use of a damping element
of relatively large dimensions and the transmission of large relative
mutual rotations of the rings.
In applications where harder spring characteristics are desired,
the damping element preferably connects two radially spaced apart
opposing surfaces of the two rings. In such an embodiment, the
damping element is preferably rotation- symmetrical and, thus,
especially well supported against deformations caused by centrifugal
forces.
During the intended application of a torsion coupling in
accordance with the invention, the radial bearing may be especially
well protected from axial forces, when the bearing and the damping
element are positioned in a common radial plane. This is also
advantageous with respect to a size reduction of the coupling, which
is desired for economic reasons.
Embodiments wherein the radial bearing is a slide bearing are
preferred for their advantageous, especially short radial length. On
the other hand, if sufficient space is available in radial direction,
the use of a deep-groove ball bearing is preferred. Deep-groove ball
bearings are available ready for installation and guarantee, in
addition to an especially good relative rotatability of the two rings,
a good guiding and support of the rings in radial direction.
The second ring may have an annular projection that is radially
spaced apart from and surrounds that leg of the U-shaped first ring,
which radially outwardly surrounds the second ring. The radial gap

20440~
resulting from the radial spacing of the annular protrusion and the
first ring is at least partly divided by a third ring into a pair of
second chambers, which second chambers at least partially surround
each other in radial direction. A second radial bearing is preferably
positioned in one of the second chambers and a second damping element
is positioned in the other of the second chambers to relatively
rotatably and elastically support the third ring. All the damping
elements and radial bearings are preferably positioned in a common
radial plane whereby the radial bearings may alternate with the
damping elements in radial direction.
The last described embodiment may be generally termed a
"cascade-type" construction. This construction may be modified by the
addition of supplementary intermediate rings similar to the third ring
in the manner described above.
The invention will now be explained by way of example only and
with reference to the following drawings, wherein:
Fig. 1 shows a half axial cross-section of a flexible torsion
coupling, which is used in a torsion damper and wherein two rings are
connected by a damping element which interconnects axially spaced
apart surfaces of the rings;
Fig. 2 is a half axial cross-section of an embodiment similar to
the one shown in Figure 1, wherein the radial bearing is a slide
bearing;
Fig. 3 illustrates a half axial cross-section of an embodiment
similar to the one shown in Figure 2, wherein the damping element
connects radially spaced apart surfaces of the two rings; and
Fig. 4 shows a half axial cross-section of a cascade-type
embodiment of a flexible torsion coupling in accordance with the
invention.

_ 4 _ 2044094
A preferred embodiment of a flexible torsion coupling in accordance with
the invention as shown in Figure 1 is integrated into a fly-wheel torsion damper, which is
affixed to an end of a crank-shaft 13 of an internal combustion engine (not illustrated) and
includes an inertia ring or fly-wheel ring 14 and a pulley 15.
The flexible torsion coupling generally includes a first ring 1, which has an
axially open U-shaped cross-section. The space defined by the U-shaped section is partially
divided by a second ring 2 into a pair of radially inner and outer first chambers 5 and 6,
whereby the outer chamber 6 partially surrounds the inner charnber 5. Second ring 2 is
rigidly connected with pulley 15. A radial bearing 4 is positioned in the radially inner first
chamber 5, which bearing is a deep-groove ball bearing and relatively rotatably supports
the second ring 2 on the radially inwardly located leg 20 of the U-shaped profile of the first
ring. Thus, the pulley 15 is also supported in radial direction and may therefore be used
for the take up of belt transmitted forces, since relative radial displacements of the pulley
15 in relation to shaft 13 are prevented by second ring 2 and radial bearing 4.
An annular`damping element 3 is positioned in second chamber 6. Damping
element 3 is made of rubber-elastic material and connects two axially spaced apart opposing
surfaces of the first and second rings 1,2. Damping element 3 axially connects first and
second rings 1 and 2. Ring portion 2a of second ring 2 is relatively non-rotatably
connected therewith. It will be readily apparent to the art skilled person that this
connection may be achieved by press-fitting or welding. The radially extending sections
of damping element 3 extending between the second ring 2 and the ring portion 2a provides
for an additional contact surface and, thus, improved fixation of the damping element.
Fly-wheel ring 14 is of L-shaped cross-section and has an axially extending leg 18, which
is radially spaced apart from and connected with first ring 1 by a fly-wheel damping
element or damping layer 19.
c ~

- 4a - 2 0 4 4 0 9 4
The embodiment shown in Figure 2 is similar in construction to the one
described above. However, instead of the deep-groove ball bearing, a slide bearing is used
in ~is embodiment. The slide bearing includes a bearing sleeve 4.1, which is rigidly
affixed to the second ring 2 and relatively rotatably engages the inner surface of the radially
S outer axially extending leg 21 of the U-shaped first ring

20~034
1. The space taken up by the coupling in radial direction is thereby
comparatively reduced.
The embodiment shown in Figure 3 is similar in construction to
the one described immediately above. However, in contrast to the
previous embodiment, wherein axially opposite surfaces are connected
by damping element 3, a damping element 3.1 relatively rotatably and
elastically connects radially opposite surfaces of the first and
second rings 1 and 2. The damping element 3.1, the slide bearing
sleeve 4.1 and the pulley 15 are positioned in a common radial plane.
Relative radial displacements of these parts of the coupling are
therefore counteracted during the intended uses of the coupling.
Figure 4 shows a schematic illustration of a coupling in
accordance with the invention having a cascade-type construction. In
this embodiment, as in all the above described embodiments, the outer
leg 21 of the U-shaped cross-section of the first ring 1 radially
outwardly surrounds the second ring 2. However, second ring 2 further
includes an annular protrusion 7, which is radially outwardly spaced
from and surrounds the outer axially extending leg 21 of the first
ring 1. The resulting radial gap between the annular protrusion 7 and
the outer leg 21 of the first ring 1 is at least partially separated
by a third ring 8 into a second pair of radially inner and outer
chambers 10,9, whereby second radially outer chamber 9 at least
partially surrounds second radially inner chamber 10. A second radial
bearing 11 is positioned in second outer chamber 9 and a second
damping element 12 for the rotatably elastic supporting of the third
ring 8 is positioned in the second inner chamber 10.
Thus, damping elements and deep-groove ball bearings alternate in
radial direction in this embodiment. This substantially prevents an
eccentric compensation movement of the fly-wheel ring 14 relative to
shaft 13 upon introduction of belt-transmitted forces. Furthermore,
it is possible to include supplementary U-shaped intermediate rings
such as third ring 8 and to affix additional fly-wheel rings 16,17 to

20~409~
second ring 2 and third ring 8 and to the intermediate rings. These
additional fly-wheel rings may also be used for the introduction of
belt-transmitted forces into the flexible torsion coupling.

Dessin représentatif
Une figure unique qui représente un dessin illustrant l'invention.
États administratifs

2024-08-01 : Dans le cadre de la transition vers les Brevets de nouvelle génération (BNG), la base de données sur les brevets canadiens (BDBC) contient désormais un Historique d'événement plus détaillé, qui reproduit le Journal des événements de notre nouvelle solution interne.

Veuillez noter que les événements débutant par « Inactive : » se réfèrent à des événements qui ne sont plus utilisés dans notre nouvelle solution interne.

Pour une meilleure compréhension de l'état de la demande ou brevet qui figure sur cette page, la rubrique Mise en garde , et les descriptions de Brevet , Historique d'événement , Taxes périodiques et Historique des paiements devraient être consultées.

Historique d'événement

Description Date
Inactive : CIB de MCD 2006-03-11
Inactive : CIB de MCD 2006-03-11
Le délai pour l'annulation est expiré 2001-06-07
Lettre envoyée 2000-06-07
Accordé par délivrance 1995-01-17
Demande publiée (accessible au public) 1991-12-10
Toutes les exigences pour l'examen - jugée conforme 1991-06-07
Exigences pour une requête d'examen - jugée conforme 1991-06-07

Historique d'abandonnement

Il n'y a pas d'historique d'abandonnement

Historique des taxes

Type de taxes Anniversaire Échéance Date payée
TM (brevet, 7e anniv.) - générale 1998-06-08 1998-04-23
TM (brevet, 8e anniv.) - générale 1999-06-07 1999-05-14
Titulaires au dossier

Les titulaires actuels et antérieures au dossier sont affichés en ordre alphabétique.

Titulaires actuels au dossier
CARL FREUDENBERG
Titulaires antérieures au dossier
JURGEN EICHHORN
RAINER-HORST ANDRA
Les propriétaires antérieurs qui ne figurent pas dans la liste des « Propriétaires au dossier » apparaîtront dans d'autres documents au dossier.
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Description du
Document 
Date
(yyyy-mm-dd) 
Nombre de pages   Taille de l'image (Ko) 
Page couverture 1995-01-16 1 18
Description 1995-01-16 7 238
Abrégé 1995-01-16 1 18
Abrégé 1995-01-16 1 18
Revendications 1995-01-16 4 137
Dessins 1995-01-16 4 76
Dessin représentatif 1999-08-22 1 20
Avis concernant la taxe de maintien 2000-07-04 1 178
Taxes 1996-04-29 1 67
Taxes 1997-04-30 1 65
Taxes 1995-05-04 1 105
Taxes 1994-05-01 1 52
Taxes 1993-06-02 1 64
Demande de l'examinateur 1993-08-03 1 58
Correspondance de la poursuite 1992-05-24 4 98
Correspondance de la poursuite 1993-12-01 7 270
Courtoisie - Lettre du bureau 1991-11-27 1 42
Correspondance reliée au PCT 1991-09-19 2 44
Correspondance reliée au PCT 1994-10-18 1 27