DEVICE FOR TRANSMITTING TORQUE

Abstract

A device for transmitting torque includes a hydrodynamic torque converter having a turbine and a pump, as well as a friction clutch that is connected in parallel to the torque converter, having a first and a second frictional segment. The first frictional segment is integrated with the pump, and the second frictional segment is integrated with the turbine. A ring-shaped frictional segment, on which the frictional elements may be brought into engagement with each other axially, and a ring-shaped flow segment, on which vanes of the pump and of the turbine are located opposite each other axially, are matched with one another in their dimensions, in order to realize a balanced transmission behavior.

Claims

1-10. (canceled)

11. A hydrodynamic torque converter, comprising: an axis of rotation; a pump including a pump housing and at least one pump vane; a turbine including a turbine housing and at least one turbine vane; a friction clutch including a ring-shaped frictional segment including: a first segment integrated with the pump housing; and, a second segment integrated with the turbine housing; a torus-shaped chamber formed in part by the at least one pump vane and the at least one turbine vane; and, a flow section located: axially between the at least one pump vane and the at least one turbine vane; and, radially outward of the torus-shaped chamber, wherein: the turbine housing is axially displaceable in an axial direction to: engage the first and second segments; close the friction clutch; and, non-rotatably connect the pump housing and the turbine housing; the ring-shaped frictional segment includes a mean radius, and a surface area in the axial direction; the flow segment includes a mean radius, and a surface area in the axial direction; respective values for the mean radius of the ring-shaped frictional segment, the surface area of the ring-shaped frictional segment, the mean radius of the flow segment, and the surface area of the flow segment are calculated to fit within a range of values for a ratio calculated using the mean radius of the ring-shaped frictional segment, the surface area of the ring-shaped frictional segment, the mean radius of the flow segment, and the surface area of the flow segment; and, the mean radius of the ring-shaped frictional segment and the mean radius of the flow segment are measured from the axis of rotation.

12. The hydrodynamic torque converter of claim 11, wherein: the ratio=(the mean radius of the ring-shaped frictional segment*the surface area of the ring-shaped frictional segment)/(the mean radius of the flow segment*the surface area of the flow segment).

13. The hydrodynamic torque converter of claim 12, wherein the ratio is at least 0.3 and is no greater than 2.4;

14. The hydrodynamic torque converter of claim 12, wherein the ratio is at least 0.5 and is no greater than 2.0.

15. The hydrodynamic torque converter of claim 12, wherein the ratio is at least 0.8 and is no greater than 1.6.

16. A hydrodynamic torque converter, comprising: an axis of rotation; a pump including a pump housing and at least one pump vane; a turbine including a turbine housing and at least one turbine vane; a friction clutch including a ring-shaped frictional segment including: a first segment integrated with the pump housing; and, a second segment integrated with the turbine housing; a torus-shaped chamber formed in part by the at least one pump vane and the at least one turbine vane; a flow section located: axially between the at least one pump vane and the at least one turbine vane; and, radially outward of the torus-shaped chamber; and, a turbine hub connected to the turbine housing and arranged to connect to a shaft, wherein: the turbine housing is axially displaceable in an axial direction to: engage the first and second segments; close the friction clutch; and, non-rotatably connect the pump housing and the turbine housing; the ring-shaped frictional segment includes an outside radius and an inside radius; the flow segment includes an outside radius and an inner radius; the turbine hub includes an inner radius; respective values for the outside and inside radii of the ring-shaped frictional segment, the outer and inner radii for the flow segment, and the inner radius of the turbine hub are calculated according to a range of values for a ratio calculated using the outside and inside radii of the ring-shaped frictional segment, the outer and inner radii for the flow segment, and the inner radius of the turbine hub; and, the outside and inside radii of the ring-shaped frictional segment, the outer and inner radii for the flow segment, and the inner radius of the turbine hub are measured from the axis of rotation.

17. The hydrodynamic torque converter of claim 16, wherein: the ratio=[(the outside radius of the ring-shaped frictional segment.sup.2−the inner radius of the turbine hub.sup.2)*(the outside radius of the ring-shaped frictional segment+the inside radius of the ring-shaped frictional segment)*0.12]/(the outer radius of the flow segment−the inner radius of the flow segment)*(the outer radius of the flow segment+the inner radius of the flow segment).sup.2

18. The hydrodynamic torque converter of claim 17, wherein the ratio is at least 0.3 and is no more than 2.0.

19. The hydrodynamic torque converter of claim 17, wherein the ratio is at least 0.4 and is no greater than 1.6.

20. The hydrodynamic torque converter of claim 17, wherein the ratio is at least 0.5 and is no greater than 1.0.

21. A hydrodynamic torque converter, comprising: an axis of rotation; a pump including a pump housing and at least one pump vane; a turbine including a turbine housing and at least one turbine vane; a friction clutch including a ring-shaped frictional segment including: a first segment integrated with the pump housing; and, a second segment integrated with the turbine housing; a torus-shaped chamber formed in part by the at least one pump vane and the at least one turbine vane; and, a flow section located: axially between the at least one pump vane and the at least one turbine vane; and, radially outward of the torus-shaped chamber, wherein: the turbine housing is axially displaceable in an axial direction to: engage the first and second segments; close the friction clutch; and, non-rotatably connect the pump housing and the turbine housing; the ring-shaped frictional segment includes a surface area in the axial direction; the flow segment includes a surface area in the axial direction; and, respective values for the surface area of the ring-shaped frictional segment and the surface area of the flow segment are calculated to fit within a range of values for a ratio calculated using the surface area of the ring-shaped frictional segment and the surface area of the flow segment.

22. The hydrodynamic torque converter of claim 21, wherein: the ratio=the surface area of the ring-shaped frictional segment/the surface area of the flow segment.

23. The hydrodynamic torque converter of claim 22, wherein: the ratio is at least 0.3 and is no greater than 2.3;

24. The hydrodynamic torque converter of claim 22, wherein: the ratio is at least 0.4 and is no greater than 1.6.

25. The hydrodynamic torque converter of claim 22, wherein: the ratio is at least 0.6 and is no greater than 1.4.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0026] The invention will be explained in greater detail below on the basis of figures. The figures show the following:

[0027] FIG. 1 is a partial cross-section through a device for transmitting torque.

[0028] FIG. 1 shows device 100 for transmitting torque around axis of rotation 105. By way of example, input side 110 and output side 115 of device 100 are provided. Device 100 is intended in particular for use in a drivetrain in a motor vehicle (not shown). Input side 110 may be connected in particular to a drive motor, for example an internal combustion engine, and output side 115 may be connected to a transmission. Device 100 includes hydrodynamic torque converter 120 and friction clutch 125, which are both positioned parallel to one another between input side 110 and output side 115.

[0029] Torque converter 120 includes pump 130 and turbine 135. Pump 130 includes pump vanes 140 and turbine 135 includes turbine vanes 145, which are opposite each other axially. In an example embodiment, diffuser, or stator, 150 with guide vanes 155 is provided, which is located on a predetermined radial section between pump vanes 140 and turbine vanes 145. Pump vanes 140 and turbine vanes 145 are set up to be coupled hydrodynamically by means of a fluid, in order to transmit torque. The fluid usually includes an oil. Pump vanes 140 are attached on an axial side to pump housing 160, and turbine vanes 145 are attached on an axial side to turbine housing 165. Pump housing 160 and turbine housing 165 face away from one another axially in reference to vanes 140 and 145. Between housings 160 and 165 a flow chamber is thus defined, in which the fluid flows between pump vanes 140, turbine vanes 145 and guide vanes 155.

[0030] On sides facing one another axially, pump vanes 140 and turbine vanes 145 have recesses on axial sides facing one another, which define torus-shaped chamber 170, referred to hereinafter as the inner torus, around axis of rotation 105. Guide vanes 155 are located on the radial inner side of inner torus 170. Radially outside of inner torus 170. flow section 175 is formed, which is located axially between sides of pump vanes 140 and turbine vanes 145 that face one another. Flow section 175 is usually ring-shaped around axis of rotation 105, and has inner radius rsi and outer radius rsa. Mean flow radius rs of flow section 175 is defined here as the arithmetic mean between inner radius rsi and outer radius rsa. The axial surface of a circular ring between radii rsi and rsa is called the cross section of flow section 175 or surface of flow section 175 in the axial direction, and is identified as As.

[0031] In the depicted embodiment, vibration damper 180 is provided between turbine 135 and output side 115, in order to damp rotational non-uniformities. Damper 180 may also be designed as necessary, for example, as a series torsion damper, and/or may include an absorber and/or a centrifugal pendulum (not shown in FIG. 1).

[0032] Friction clutch 125 includes frictional segment 185 and frictional segment segment 190, which are located on different axial sides of ring-shaped frictional segment 195. Frictional segment 185 is integrated with pump 130,in particular pump housing 160, and frictional segment 190 is integrated with turbine 135, in particular with turbine housing 165. One of frictional segments 185 or 190 may include a friction element. Frictional segment 195 extends in a ring shape around axis of rotation 105, between inner radius rri and outer radius rra. Located between rri and rra is mean radius rr of frictional segment 195. A circular ring having inner radius rri and outer radius rra around axis of rotation 105 defines surface area Ar of frictional segment 195 in the axial direction.

[0033] For example, during the process of starting to drive a motor vehicle, input side 110 with pump 130 rotates at a certain speed, while output side 115 with turbine 135 is still standing still. The greater the difference in speed of rotation between pump 130 and turbine 135, the greater the torque that is transmissible via hydrodynamic torque converter 120. When the motor vehicle starts to drive off, a rotary motion of turbine 135 is accelerated and a difference in speed between pump 130 and turbine 135 decreases. The torque transmissible via torque converter 120 likewise decreases as a result, so that turbine 135 cannot reach the speed of pump 130 hydrodynamically. To adjust the speeds to one another, friction clutch 125 may be engaged. To this end, frictional segments 185 and 190 are pressed against one another axially. In the depicted embodiment, turbine 135 is placed so that the turbine is movable axially on a shaft which is connected to output side 115. If turbine 135 is pressed axially in the direction of pump 130, friction clutch 125 is engaged. A movement of turbine 135 in the opposite axial direction disengages friction clutch 125.

[0034] The axial movement, or the exertion of an axial force on turbine 135, may occur in particular hydrodynamically. In the depicted embodiment, turbine 135 is sealed at turbine hub 196 by means of shaft sealing ring 198 relative to shaft S, which is connected to output side 115. An overpressure of the fluid on one of the axial sides of turbine 135 drives turbine 135 in the corresponding axial direction. Through the use of an elastic element (not shown), turbine 135 may also be pre-tensioned in an axial direction. An increased hydraulic pressure on the respective other side of turbine 135 can counteract the spring force. In one embodiment (not shown), the hydraulic pressure is controlled specifically, in particular by means of a pump and possibly a valve. In another embodiment, the hydraulic pressure may also be built up by centrifugal forces.

[0035] Flow segment 175 and frictional segment 195 are matched to one another in such a way that predetermined value ratios result. This enables the transmission capabilities for torque of torque converter 120 and of friction clutch 125 to be adjusted to one another. In particular, a process of engaging the friction clutch 125 proceeds better.

REFERENCE LABELS

[0036] 100 device [0037] 105 axis of rotation [0038] 110 input side [0039] 115 output side [0040] 120 hydrodynamic torque converter [0041] 125 friction clutch [0042] 130 pump [0043] 135 turbine [0044] 140 pump vane [0045] 145 turbine vane [0046] 150 diffuser [0047] 155 guide vane [0048] 160 pump housing [0049] 165 turbine housing [0050] 170 inner torus [0051] 175 flow segment [0052] 180 vibration damper [0053] 185 frictional segment [0054] 190 frictional segment [0055] 195 frictional segment [0056] 196 turbine hub [0057] 198 sealing ring [0058] S shaft