The pump wheel shell 22 and the pump wheel vanes together form a pump wheel 26, which cooperates with a turbine wheel 30, comprising a turbine wheel shell 28 and turbine wheel vanes, and with a stator 32 equipped with stator vanes. The pump wheel 26, the turbine wheel 30, and the stator 32 form a hydrodynamic circuit 34 in the conventional manner.
The stator 32 is mounted on a freewheel 36, which is supported axially against the pump wheel hub 24 by an axial bearing 38 permeable to the fluid medium and is connected nonrotatably but with freedom of relative movement in the axial direction to a support shaft 42 by means of a set of teeth 40. The support shaft is located radially inside the takeoff-side housing hub 24 and forms together with it a channel 43. The support shaft 42, designed as a hollow shaft, surrounds the gearbox input shaft 19, serving as the takeoff 18, to form an essentially ring-shaped channel 44. The gearbox input shaft has two axial passages 46, 48, offset from each other in the radial direction, for fluid medium. The first axial passage 46 leads to a deflection chamber 92 on the drive-side end 94 of the gearbox input shaft 19, whereas the second axial passage 48 terminates at a plug 98 shortly before reaching the drive-side end 94 of the gearbox input shaft 19 and then opens radially outward by way of a radial connection 96.
The axial passages 46, 48, like the channel 44 and/or the channel 43, are connected by flow lines 72-74 and/or 103 to a fluid distributor 82, which can be connected to a supply source 80 to receive fluid medium and to a reservoir 84, into which the fluid medium can be discharged. The latter can be connected to the supply source 80 by a connecting line 86.
The gearbox input shaft 19 has a set of teeth 50, by which it holds a torsion damper hub 52 of a torsional vibration damper 54 nonrotatably but with freedom of axial movement. The torsion damper hub 52 is supported on one side against the previously mentioned freewheel 36 by an axial bearing 58, and on the other side it can come to rest against the housing cover 20. The torsion damper hub 52, furthermore, carries a piston 62 of a clutch device 66, designed as a bridging clutch 64. The piston 62 is sealed off against the torsion damper hub 52 by a radially inner piston seal 68 and against the housing cover 20 by a radially outer piston seal 70.
On the radially inner side of the torsion damper hub 52, a seal 71 is provided, which is supported on the other side against the gearbox input shaft 19 and acts between the radial passages 88, 90 provided in the torsion damper hub 52. The drive-side radial passage 88 cooperates with the deflection chamber 92, the first axial passage 46, and the first flow line 72, to form a first supply line 75 for fluid medium, whereas the takeoff-side radial passage 90 cooperates with the radial connection 96, the second axial passage 48, and the second flow line 73 to form a second supply line 76. Finally, to form a third supply line 78, a flow passage 100 axially between the axial bearing 58 and the freewheel 36 cooperates with the channel 44 and the flow line 74, and/or a flow passage 102 axially between the freewheel 36 and the axial bearing 38 cooperates with the channel 43 and the flow line 103.
Fluid medium introduced via the first supply line 75 from the fluid distributor 82 arrives in a drive-side pressure space 105, located between the housing cover 20 and the piston 62. When there is positive pressure in this space, it acts on the drive side 107 of the piston 62. Fluid medium introduced via the second supply line 76 from the fluid distributor 82 arrives, in contrast, in a takeoff-side pressure space 112, located between the piston 62 and a partition wall 110, which is free to move axially relative to the piston. When there is positive pressure in this space, it acts on a takeoff side 114 of the piston 62.
The partition wall 110 can be designed with axial elasticity. It is centered by its radially inner end 115 on the torsion damper hub 52 by sealing 160, where this sealing 160 is designed as a gap seal 116. The radially outer end 117 of the partition wall 110 serves as an antitwist device 162, projecting axially into an area between the piston 62 and the first clutch element 122 of a clutch 120. So that the fluid medium can flow easily, the partition wall 110 is provided with spacers 124 on the side facing the piston 62. Between them, the spacers form first flow channels 125, which are distributed around the circumference and extend in the radial direction between the piston 62 and the partition wall 110. Alternatively or in addition, the piston 62 can be designed with nubs 126, so that, in this way, second flow channels 127 integrated into the piston 62 are obtained. As a result, a pressure area 129 is formed in the piston 62.
On the interior side of an axial section 128 of the housing cover 20, a set of teeth 130 is provided for the radially outer clutch elements 132, referred to in the following in brief as “outer clutch elements”, to which the previously mentioned first clutch element 122 and a last clutch element 134, which has a larger cross section and is therefore stiffer, belong. The latter element is supported axially on the housing cover 20 by a back-up ring 136. Because of the set of teeth 130, the outer clutch elements 132 are connected nonrotatably to the housing 5 and thus to the drive 11.
Under the action of the piston 62, the outer clutch elements 132 can be brought into working connection with the radially inner clutch elements 138, referred to in the following in brief as “inner clutch elements”, where a friction area 140 of a clutch 120 serving to transmit torque is created between the friction linings and friction surfaces of the clutch elements 132, 138. The inner clutch elements 138 are connected nonrotatably to an input part 146 of the torsional vibration damper 54 by way of a set of teeth 142 on a carrier 144. By means of this input part, the torque can be transmitted via the set of teeth 50 to the gearbox input shaft 19. Thus the inner clutch elements 138 are connected to the takeoff 18 by way of the torsional vibration damper 54. When the clutch elements 132, 138 are separated from each other, however, torque introduced by the housing 5 is transmitted via the hydrodynamic circuit 34 to the turbine wheel 30 and from that by means of a connection 146 to the torsional vibration damper 54, from which the torque in turn is transmitted onward to the gearbox input shaft 19 and thus to the takeoff 18. If a torsional vibration damper 54 is not provided, the inner clutch elements 138 can be connected directly to the takeoff 18 in either of the two operating states.
In regard to the partition wall 110 it only remains to be noted that, because of the engagement of its radially outer end 117 axially between the piston 62 and the first clutch element 122, it participates in the transmission of axial force from the piston 62 to the friction area 140 of the clutch 120. Preferably in this case the partition wall 110 is provided with axial elasticity and is therefore designed especially as a diaphragm-like element. In addition, the partition wall 110 can be connected nonrotatably to the set of teeth 130 of the outer clutch elements 132 by way of a set of teeth 148 on its radially outer end 117.
To close the bridging clutch 64 and thus to engage it, positive pressure versus the takeoff-side pressure space 112 is built up in the drive-side pressure space 105 by way of the first supply line 75. As a result, the piston 62 and the partition wall 110 are both shifted toward the clutch 120 and thus exert an axial force on the clutch elements 132, 138. In this operating state, the partition wall 110 is thus pressed by the piston 62 against the first clutch element 122. Simultaneously, the takeoff-side pressure space 112 is being supplied with fluid medium through the second supply line 76 to cool the friction area 140 of the clutch 120. Thanks to the spacers 124 and/or the profiling 126, the medium flowing in from the second supply line 76 can travel radially outward via the flow channels 125, 127 in the pressure space 112 and then flow away via the set of teeth 148 of the partition wall 110 directly into the set of teeth 130 of the outer clutch elements 132. The set of teeth 148 thus acts as the only flow passage 150 for the fluid medium between the takeoff-side pressure space 112 and a cooling space 220, in which the clutch 120 is installed, so that, every time fluid medium passes between these two spaces 112, 220 of the fluid-filled clutch arrangement 3, the clutch 120 is subjected to the forced flow of the fluid. If the fluid-filled clutch arrangement 3 is designed as a hydrodynamic torque converter, the cooling space 220 acts simultaneously as the hydrodynamic circuit 34.
After entering the set of teeth 130 of the outer clutch elements 132, the fluid medium is conveyed axially onward within the toothed area, but it will never be conveyed farther than the axial area of the last clutch element 134 and/or of the back-up ring 136 as long as appropriate sealing measures have been taken on at least one of these components and/or in the area of the set of teeth 130. In this way, the only possibility remaining to the fluid medium is to flow radially inward through the friction area 140 of the clutch 120 between the clutch elements 132 and 138 into the cooling space 220, and as a result it cools the friction area 140 in a highly efficient manner.
From the cooling space 220, the fluid medium travels via the flow passage 100 and/or 102 and thus via the third supply line 78 back to the fluid distributor 82.
To open the bridging clutch 64 and thus to disengage it, the second supply line 76 and thus the takeoff-side pressure space 112 are subjected to positive pressure versus the drive-side pressure space 105, and thus the piston 62 is shifted toward the housing cover 20 to release the axial force transmitted to the clutch elements 132, 138. The supply of the takeoff-side pressure space 112 with fluid medium from the second supply line 76 has the effect that the partition wall 110 remains in contact axially with the first clutch element 122, whereas the piston 62 completes its shifting movement toward the housing cover 20. In this operating state as well, therefore, the set of conditions according to which the fluid medium can flow away only via the set of teeth 148 of the partition wall 110 from the takeoff-side pressure space 112 still remains in effect. The fluid thus immediately enters the set of teeth 130 of the outer clutch elements 132, so that the set of teeth 148 continues to act as a flow passage 150 for the fluid medium between the takeoff-side pressure space 112 and the hydrodynamic circuit 34.
While the bridging clutch 64 is being opened or after the bridging clutch 64 has been opened, the fluid medium will first, after entering the set of teeth 130 of the outer clutch elements 132, be conducted axially onward over at least a part of the toothed area. It will then flow away through the friction area 140 of the clutch 120, through the cooling space 220, and return to the fluid distributor 82 via the flow passage 100 and/or 102 and thus via the third supply line 78.
As a result of the partition wall 110, therefore, regardless of the operating state of the bridging clutch 64, it is ensured that the flow passage 150 will always represent the only flow connection at the time in question between the takeoff-side pressure space 112 and the cooling space 220, as a result of which a forced flow exclusively by way of the clutch 120 is created between these two spaces 112, 220 of the fluid-filled clutch arrangement 3.
To ensure the trouble-free flow of the fluid medium through the friction area 140 of the clutch 120, grooves 174 are provided within the area over which the friction area 140 extends, preferably in the friction linings 172.
In a departure from the way in which the flow is guided in the variants described up to now, it is also possible, of course, when the bridging clutch 64 is being opened or after the bridging clutch 64 has been opened, for the fluid medium to be supplied from the fluid distributor 82 by way of the third supply line 78, so that the medium, after passing through the cooling space 220 and the clutch 120, arrives via the flow passage 150 in the takeoff-side pressure space 112. From there it flows radially inward and returns to the fluid distributor 82 by way of the second supply line 76. When this flow direction is chosen, of course, the pressure in the cooling space 220 will be higher than that in the takeoff-side pressure space 112, and this will result in the axial displacement of the partition wall 110 toward the piston 62 and thus the separation of the partition wall 110 from the adjacent first clutch element 122. This means that a gap 222 can form between the partition wall 110 and the first clutch element 122. As a result, there can be some residual leakage from the cooling space 220, in that the fluid can seep into the gap 222. Because the bridging clutch 64 is open, however, this does not have any negative effect, because the clutch 120 to be cooled is not being heated to any significant degree in the absence of friction. In spite of the gap 222, furthermore, most of the fluid flowing through the flow passage 150 will still arrive in the takeoff-side pressure space 112.
Because of this situation, it is possible to fasten the partition wall 110 to the takeoff-side 114 of the piston 62 by means of permanent connections 151. Then, although the partition wall 110 remains always a constant distance away from the position 62, it will form the previously mentioned gap 222 between the partition wall 110 and the adjacent first clutch element 122 when the piston moves away from the clutch 120. In the design according to
A permanent connection 151 in the area of each spacer 124 but produced by a different connection method is shown in
An arrangement similar to
Another design of this type is shown in
Preferably in the same radial area but with a different design,
So far, only embodiments of the fluid-filled clutch arrangement 3 with three supply lines 75, 76, and 78 have been discussed, referred to in brief as “three-line systems”. In
The only difference involves the flow route for supplying the takeoff-side pressure space 112 with fluid medium. When the bridging clutch 64 is closed, the fluid medium originates from the drive-side pressure space 105, namely, via a first connection 208, provided in the piston 62. This connection acts as part of a throttle 216 and thus allows only a limited volume flow rate to pass from the drive-side pressure space 105 into the takeoff-side pressure space 112.
The drive-side pressure space 105 is supplied by the fluid arriving from the fluid distributor 82 via the flow line 212, which is assigned to the first supply line 202 and which leads to the center bore 210 in the gearbox input shaft 19. The fluid then flows via the deflection chamber 92, also assigned to the first supply line 202, and arrives in the drive-side pressure space 105 from the deflection chamber via channels 224 in the drive-side housing hub 15. Because of the positive pressure present there in this operating state versus the takeoff-side pressure space 112, the fluid medium is conveyed from the drive-side pressure space 105 via a first connection 208 into the takeoff-side pressure space 112. In this operating state, a valve 206, which is integrated into the piston 62 and which controls a second connection 214 between the pressure spaces 105 and 112 and thus serves as another part of the throttle 216, is closed to block off the second connection 214.
The fluid medium which has thus arrived in the takeoff-side pressure space 112 then flows under the effect of centrifugal force radially outward within the pressure space 112, and from there it flows in the previously described manner via the flow passage 150 and the set of teeth 130 on the housing cover 20 as forced flow to the friction area 140 of the clutch 120. From there, after it has been used in the cooling space 220, it returns to the fluid distributor 82 via the second supply line 204.
So that the bridging clutch 64 can be at least partially opened or so that the bridging clutch 64 can be opened completely, the second supply line 204 is subjected to a positive pressure versus the drive-side pressure space 105, whereupon the fluid medium arrives via the clutch 120 and the set of teeth 130 assigned to the outer clutch elements 132 in the area over which the partition wall 110 extends. It then flows away via the set of teeth 148 on the partition wall serving as a flow channel 150 for the fluid medium into the takeoff-side pressure space 112. As a result of pressure in the takeoff-side pressure space 112, which is increasing versus the drive-side pressure space 105, the piston 62 is shifted toward the housing cover 20 and thus at least partially releases the axial force being transmitted to the clutch elements 132, 138.
Because of the positive pressure in the takeoff-side pressure space 112 versus the drive-side pressure space 105, the fluid medium present in the takeoff-side pressure space 112 is conveyed via the first connection 208 into the drive-side pressure space 105. Simultaneously, the positive pressure in the takeoff-side pressure space 112 causes the valve 206 to open, so that the second connection 214 assigned to it is also released. Fluid medium now flows at a greater rate via the connections 208 and 214 into the drive-side pressure space 105, from which it then returns to the fluid distributor 82 via the first supply line 202.
The partition wall 110 preferably has an integrated zone 228, a certain predetermined radial distance away from the axis of rotation 4 of the housing 5. This zone is provided, for example, in the radial area of the profiling 126 on the piston 62 and can be designed as a spring zone. This integrated zone 228 can, as
According to
To return to
Independently of the axial stiffness selected in a specific case, each of the designs of the partition wall 110 according to
On the basis of the interrupted profiling 238,
In contrast, the tooth root areas 243 of the set of teeth 130 provided on the axial section 128 of the housing 5 engage at least essentially without radial gaps with the tooth tip areas 241 of the associated radially outer clutch elements 132 and of the last clutch element 134, because the tooth tip areas 241 extend at least essentially right up to the associated tooth root areas 243 of the set of teeth 130 and as a result form near-contacts 248, each of which serves as a flow obstacle 250 for the fluid medium.
The last clutch element 134 serves as an axial stop for the radially outer clutch elements 132 of the clutch 120 and is positioned axially with respect to the set of teeth 130 by a back-up ring 136, inserted into a circumferential groove 252 provided in the axial section 128 of the housing 5, especially provided in the set of teeth 130. Because of its engagement in the circumferential groove 252, the back-up ring 136 acts as a fluid seal 254, by which at least most of the fluid medium arriving through the flow passages 246 is prevented from leaving the cooling space 220. The fluid medium is therefore forced to flow through the cooling space and can leave it only after passing through the clutch elements 132 and 138, after which it can flow onward into the hydrodynamic circuit 34. Because of its action as a fluid seal 254, the back-up ring 136 therefore supports the function of the near-contacts 248, which, as previously mentioned, serve as flow obstacles 250.
Thus, while there have shown and described and pointed out fundamental novel features of the invention as applied to a preferred embodiment thereof, it will be understood that various omissions and substitutions and changes in the form and details of the devices illustrated, and in their operation, may be made by those skilled in the art without departing from the spirit of the invention. For example, it is expressly intended that all combinations of those elements and/or method steps which perform substantially the same function in substantially the same way to achieve the same results are within the scope of the invention. Moreover, it should be recognized that structures and/or elements and/or method steps shown and/or described in connection with any disclosed form or embodiment of the invention may be incorporated in any other disclosed or described or suggested form or embodiment as a general matter of design choice. It is the intention, therefore, to be limited only as indicated by the scope of the claims appended hereto.
| Number | Date | Country | Kind |
|---|---|---|---|
| 10 2006 016 417.2 | Apr 2006 | DE | national |
| 10 2007 005 999.1 | Feb 2007 | DE | national |