Torque transmission device
View Patent ↗A torque transmission device, comprising a hydrodynamic component, a shiftable clutch device and a vibration damper. A turbine shell of the hydrodynamic component is connected with a damper input component of the vibration damper and/or with a turbine shell hub, which is at least indirectly supported in axial direction at a damper hub through a torque-proof connection. At least one axial support surface is provided at a face of a damper component, adjacent to the torque-proof connection in an axial direction, or of the damper hub. The face is oriented away in axial direction from the torque-proof connection. The invention is characterized in that a support element is arranged at the damper component or at the damper hub. The support element includes a support surface forming an axial protrusion, extending through adjacently arranged damper components or portions of a support.
1. A torque transmission device ( 1 ), comprising a rotation axis, a hydrodynamic component ( 2 ), a shiftable clutch device ( 3 ) and a vibration damper ( 4 ), wherein:
the vibration damper includes:
a damper input component ( 4 . 1 ) including:
a first drive disc ( 7 . 1 ) non-rotatably connected to the shiftable clutch device; and,
a second drive disc ( 7 . 2 ) non-rotatably connected to the first drive disc;
a first lateral disc ( 24 . 1 ) forming at least a portion of an output of the vibration damper; and,
a damper hub ( 9 ) non-rotatably connected to the first lateral disc, the damper hub:
forming an output of the torque transmission device ( 1 ); and,
including:
at least one first axial support surface ( 22 . 1 - 22 .n ) orthogonal to the rotation axis; and,
a support surface ( 22 . 1 - 22 .n ):
forming an axial protrusion:
extending through the first lateral disc;
aligned, in an axial direction, parallel to the rotation axis, with an opening in the first drive disc; and,
offset, in the axial direction, from the opening;
a turbine shell (T) of the hydrodynamic component ( 2 ) is non-rotatably connected with the damper input component ( 4 . 1 ) with a torque-proof connection ( 18 );
the at least one first axial support surface ( 22 . 1 - 22 .n ) is oriented away, in the axial direction, from the torque-proof connection ( 18 ); and,
the damper input component is at least indirectly supported in an axial direction, parallel to the rotation axis, at the damper hub ( 9 ) through the torque-proof connection ( 18 ).
2. The torque transmission device ( 1 ) according to claim 1 , wherein the damper hub is configured with a variable cross sectional surface in the axial direction and includes a larger cross sectional surface in the portion ( 26 . n ) forming the support surface ( 22 . 1 - 22 .n ), than in a pass through portion ( 27 .n ).
3. The torque transmission device ( 1 ) according to claim 1 , further comprising: a second lateral disc ( 24 . 2 ) and a turbine hub ( 15 ), wherein the first lateral disc ( 24 . 1 ) is connected torque proof with the damper hub ( 9 ); and the torque transmission device ( 1 ) further comprises a device ( 28 ) forming at least one second axial support surface ( 29 , 30 , 30 . 1 - 30 .n ) for at least indirectly supporting the turbine shell hub ( 15 ) at the damper hub ( 9 ), wherein the devices ( 28 ) is connected with the damper hub ( 9 ), the second lateral disc ( 24 . 2 ), or integrally configured therewith.
4. The torque transmission device ( 1 ) according to claim 3 , wherein the device ( 28 ) for at least indirectly supporting the turbine shell hub ( 15 ) at the damper hub ( 9 ) is integrally configured with the damper component ( 23 ) adjacent to the torque proof connection ( 18 ) in the axial direction or integrally configured with a support element ( 21 . 1 - 21 .n ) arranged at the damper hub ( 9 ).
5. The torque transmission device ( 1 ) according to claim 1 , wherein the vibration damper includes a second lateral disc ( 24 . 2 ) forming at least a portion of the output of the vibration damper, and the damper hub ( 9 ) is configured to extend through the first and second lateral discs ( 24 . 1 , 24 . 2 ).
6. The torque transmission device ( 1 ) according to claim 1 , wherein:
the vibration damper includes:
an intermediary flange ( 23 ); and,
a second lateral disc ( 24 . 2 ) forming at least a portion of the output of the vibration damper;
the first and second lateral discs are arranged on both sides of the intermediary flange ( 23 );
the intermediary flange ( 23 ) is adjacent, in the axial direction, to the torque proof connection ( 18 ) and is located, in the axial direction, between the turbine shell (T) and the vibration damper ( 4 ); and
the damper hub is arranged at the intermediary flange ( 23 ) and is configured to extend through the first and second lateral discs.
7. The torque transmission device ( 1 ) according to claim 1 , wherein:
the vibration damper includes:
an intermediary flange ( 23 ); and,
a second lateral disc ( 24 . 2 ) forming at least a portion of the output of the vibration damper; and
the damper hub is arranged at the intermediary flange and configured to extend through the first and second lateral discs.