Torque converter with a cover having recessed flexplate connection
US-9683644-B2 · Jun 20, 2017 · US
US9841093B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9841093-B2 |
| Application number | US-201514813992-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 30, 2015 |
| Priority date | Jul 30, 2015 |
| Publication date | Dec 12, 2017 |
| Grant date | Dec 12, 2017 |
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A torque converter, including an axis of rotation, a cover arranged to receive torque, an impeller including an impeller shell non-rotatably connected to the cover and, at least one impeller blade fixedly connected to the impeller shell, a turbine including a turbine shell and at least one turbine blade fixedly connected to the turbine shell, a stator axially disposed between the impeller and turbine shells and including at least one stator blade and a first core ring fixedly secured to the at least one impeller blade and, including at least one first flat annular surface facing the at least one turbine blade or a second core ring fixedly secured to the at least one turbine blade and, including at least one second flat annular surface facing the at least one impeller blade.
Opening claim text (preview).
What is claimed is: 1. A torque converter, comprising: an axis of rotation; a cover arranged to receive torque; an impeller including: an impeller shell non-rotatably connected to the cover; and, at least one impeller blade fixedly connected to the impeller shell; a turbine including a turbine shell and at least one turbine blade fixedly connected to the turbine shell; a stator axially disposed between the impeller and turbine shells and including at least one stator blade; a first core ring or a second core ring, the first core ring fixedly secured to the at least one impeller blade; and, including at least one first flat annular surface facing the at least one turbine blade; the second core ring fixedly secured to the at least one turbine blade and, including at least one second flat annular surface facing the at least one impeller blade, wherein a flat surface is represented by a straight line in a cross-section formed by a plane parallel to and passing through the axis of rotation, wherein the at least one first flat annular surface includes first and second surfaces orthogonal to the axis of rotation; the first core ring includes a first recess radially disposed between the first and second surfaces; and, the impeller blade includes a first tab passing through the first core ring and at least partially disposed within the first recess; or, the at least one second flat annular surface includes third and fourth surfaces orthogonal to the axis of rotation; the second core ring includes a second recess radially disposed between the third and fourth surfaces; and, the turbine blade includes a second tab passing through the second core ring and at least partially disposed within the second recess. 2. A torque converter, comprising: an axis of rotation; a cover arranged to receive torque; an impeller including: an impeller shell non-rotatably connected to the cover; and, at least one impeller blade fixedly connected to the impeller shell; a turbine including a turbine shell and at least one turbine blade fixedly connected to the turbine shell; a stator axially disposed between the impeller and turbine shells and including at least one stator blade; a first core ring or a second core ring the first core ring fixedly secured to the at least one impeller blade; and, including at least one first flat annular surface orthogonal to the axis of rotation; or, the second core ring fixedly secured to the at least one turbine blade; and, including at least one second flat annular surface orthogonal to the axis of rotation, wherein a flat surface is represented by a straight line in a cross-section formed by a plane parallel to and passing through the axis of rotation, wherein the at least one first flat annular surface orthogonal to the axis of rotation includes third and fourth flat annular surfaces orthogonal to the axis of rotation; the first core ring includes a first recess radially disposed between the third and fourth flat annular surfaces; and, the impeller blade includes a first tab passing through the first core ring and at least partially disposed within the first recess; or, the at least one second flat annular surface orthogonal to the axis of rotation includes fifth and sixth flat annular surfaces orthogonal to the axis of rotation; the second core ring includes a second recess radially disposed between the fifth and sixth flat annular surfaces; and, the turbine blade includes a second tab passing through the second core ring and at least partially disposed within the second recess.
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