The invention relates generally to a turbine piston, and more specifically to a turbine piston preloaded against an impeller shell.
Turbine pistons are known. One example is shown in commonly-assigned United States Patent Publication No. 2013/0230385.
Example aspects broadly comprise a torque converter with a cover assembly, an impeller assembly, a turbine assembly and a damper assembly. The impeller assembly includes an impeller shell drivingly connected with the cover assembly. The turbine assembly includes a shell with a clutch portion for selective driving engagement with the impeller shell. The damper assembly includes at least one cover plate, a flange for driving engagement with a transmission input shaft, and a first resilient element drivingly engaged with the at least one cover plate and the flange. The torque converter has a second resilient element for urging the turbine assembly away from the cover assembly.
In some example embodiments, the at least one cover plate is fixed to the turbine shell and the resilient element urges the at least one cover plate away from the cover assembly. In some example embodiments, the cover assembly includes a centering plate and a bushing press-fitted into the centering plate. The flange includes a hub portion installed into the bushing and rotatable relative to the bushing. In some example embodiments, the second resilient element is a diaphragm spring disposed axially between the centering plate and the flange.
In an example embodiment, the bushing includes flanged portion with a first plurality of radial castellations and the diaphragm spring includes a second plurality of radial castellations drivingly engaged with the first plurality of radial castellations for preventing relative rotation between the diaphragm spring and the bushing. In an example embodiment, the torque converter has a hardened washer disposed axially between the diaphragm spring and the flange. In an example embodiment, the torque converter has a hardened washer disposed axially between the diaphragm spring and the bushing. The bushing includes a first annular portion and the flange includes a plurality of cutouts. The hardened washer has a second annular portion matingly engaged with the bushing annular portion and a plurality of tabs installed in the flange cutouts for preventing relative rotation between the hardened washer and the flange.
In some example embodiments, the second resilient element is a diaphragm spring disposed axially between the cover plate and the flange. In an example embodiment, the at least one cover plate includes a radially inwardly extending portion and the diaphragm spring is disposed axially between the inwardly extending portion and the flange. In an example embodiment, the radially inwardly extending portion includes a plurality of first tabs and the diaphragm spring includes a plurality of second tabs engaged with the plurality of first tabs for preventing relative rotation between the diaphragm spring and the cover plate.
In some example embodiments, the second resilient element is disposed axially between the flange and the turbine shell. In an example embodiment, the second resilient element is fixed to the turbine shell. In an example embodiment, the torque converter has a thrust washer disposed axially between the at least one cover plate and the cover assembly.
Other example aspects broadly comprise a torque converter with an outer shell including a cover fixed to an impeller shell and a turbine shell including a clutch portion preloaded against the impeller shell. In an example embodiment, the impeller shell and the turbine shell comprise respective torus portions and the clutch portion is disposed radially outside of the torus portions. In an example embodiment, the torque converter has a stator disposed axially between the impeller shell and the turbine shell. In an example embodiment, the torque converter has a damper assembly disposed in a torque path between the turbine shell and a transmission input shaft. In some example embodiment, the cover shell is arranged for driving engagement with a prime mover. In an example embodiment, the turbine shell clutch portion is preloaded against the impeller shell by a resilient element. In an example embodiment, the resilient element reacts against the cover shell.
The nature and mode of operation of the present invention will now be more fully described in the following detailed description taken with the accompanying drawing figures, in which:
At the outset, it should be appreciated that like drawing numbers appearing in different drawing views identify identical, or functionally similar, structural elements. Furthermore, it is understood that this invention is not limited only to the particular embodiments, methodology, materials and modifications described herein, and as such may, of course, vary. It is also understood that the terminology used herein is for the purpose of describing particular aspects only, and is not intended to limit the scope of the present invention, which is limited only by the appended claims.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood to one of ordinary skill in the art to which this invention belongs. Although any methods, devices or materials similar or equivalent to those described herein can be used in the practice or testing of the invention, the following example methods, devices, and materials are now described.
The following description is made with reference to
Converter 100 also includes damper assembly 116 disposed in a torque path between the turbine shell and a transmission input shaft (not shown). The damper assembly includes cover plates 118 and 120 fixed together at rivet 121, flange 122, and resilient elements (i.e., coil springs) 124 and 125. Flange 122 is for driving engagement with a transmission input shaft (not shown) at spline portion 126, for example. Springs 124 and 125 are drivingly engaged with cover plates 118 and 120, and flange 122. That is, the springs transfer torque between the cover plates and flange. Cover plate 118 is fixed to the turbine shell at rivet 123.
Torque converter 100 further includes resilient element (i.e., diaphragm spring) 130 for urging turbine assembly 110 away from cover assembly 102. In other words, clutch portion 114 is preloaded against impeller shell 106. Cover assembly 102 includes centering plate 132, fixed to the cover assembly at projection weld 134, and bushing 136 press-fitted into the centering plate. That is, the bushing must be forcefully installed into the centering plate such that the two are fixed together. Flange 122 includes hub portion 138 installed into the bushing and rotatable relative to the bushing.
Cover assembly 102 includes outer shell 139. Impeller shell 106 and cover shell 139 form an outer shell for torque converter 100. Element 130 reacts against the cover shell. Impeller shell 106 includes torus portion 140 with blades 142. Turbine shell 112 includes torus portion 144 with blades 146. Clutch portion 114 is disposed radially outside of the torus portions. Stator 148 is disposed axially between the impeller shell and the turbine shell. Stator 148 includes one-way clutch assembly 150, side plate 152, and thrust washer, or hydrodynamic bearing, 154 fixed to the side plate. Cover shell 139 is arranged for driving engagement with a prime mover at stud 156, for example.
The following description is made with reference to
The following description is made with reference to
The following description is made with reference to
The following description is made with reference to
The following description is made with reference to
Converter 600 also includes damper assembly 616 disposed in a torque path between the turbine shell and a transmission input shaft (not shown). The damper assembly includes cover plates 618 and 620 fixed together at rivet 621, flange 622, and resilient element (i.e., coil spring) 124. Flange 622 is for driving engagement with a transmission input shaft (not shown) at hub portion 626, for example. Spring 624 is drivingly engaged with cover plates 618 and 620, and flange 622. That is, the springs transfer torque between the cover plates and flange. Cover plate 618 is drivingly engaged with the turbine shell at spring 623.
Torque converter 600 further includes resilient element 630 for urging turbine assembly 610 away from cover assembly 602. In other words, clutch portion 614 is preloaded against impeller shell 606. Resilient element 630 is disposed axially between the flange and the turbine shell, and fixed to the turbine shell at rivet 680. Torque converter 600 includes thrust washer 682 disposed axially between cover plate 620 and the cover assembly.
Of course, changes and modifications to the above examples of the invention should be readily apparent to those having ordinary skill in the art, without departing from the spirit or scope of the invention as claimed. Although the invention is described by reference to specific preferred and/or example embodiments, it is clear that variations can be made without departing from the scope or spirit of the invention as claimed.
Filing Document | Filing Date | Country | Kind |
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PCT/US2016/013344 | 1/14/2016 | WO | 00 |
Number | Date | Country | |
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62113966 | Feb 2015 | US |