Ring element, particularly a race ring for a thrust roller bearing
View Patent ↗A ring element, particularly a thrust bearing race ring, which has a peripheral wall, through which a radial load exerting an interference fit occurs. The peripheral wall is configured such that it forms zones with a large overlap and zones with a reduced overlap that succeed each other in a peripheral direction.
1. A thrust bearing assembly, comprising:
an axis;
a housing having an inner periphery;
a gearwheel;
a first race ring;
in contact with the inner periphery of the housing;
located inward of the housing in a radial direction orthogonal to the axis; and, comprising:
an outer peripheral wall including:
a plurality of valleys; and,
a plurality of peaks;
an inner peripheral wall; and,
a front end face:
orthogonal to the axis and facing in a first axial direction parallel to the axis; and,
connecting the outer peripheral wall and the inner peripheral wall;
a second race ring in contact with the gearwheel and including a first end face orthogonal to the axis and facing a second axial direction, opposite the first axial direction; and,
a plurality of cylindrical or needle rollers disposed between the front end face and the first end face in the first axial direction, wherein:
the outer peripheral wall, includes:
a first annular step:
in contact with the housing; and,
having a first outer diameter;
a second annular step having a second outer diameter less than the first outer diameter; and,
a third annular step:
having a third outer diameter less than the second outer diameter; and,
the first annular step includes the plurality of valleys and the plurality of peaks;
at least a portion of the plurality of peaks is in contact with the housing;
the plurality of peaks extend further from the axis in the radial direction, orthogonal to the axis, than the plurality of valleys; and,
respective peaks from the plurality of peaks alternate, in a peripheral direction, with respective valleys from the plurality of valleys a spring ring engages the third annular step.
2. The thrust bearing assembly according to claim 1 , wherein the pluralities of valleys and peaks approximate a polygonal wall in that the plurality of valleys represents sides of a polygon and the plurality of peaks represents corners of the polygon.
3. The thrust bearing assembly according to claim 2 , wherein the polygonal wall includes at least three valleys and three peaks.
4. The thrust bearing assembly according to claim 1 wherein the plurality of valleys and the plurality of peaks are disposed on only one of the annular steps which approximates a polygonal contour in that the plurality of valleys represents sides of a polygon and the plurality of peaks represents corners of the polygon.
5. The thrust bearing assembly according to claim 4 , wherein the first annular step has the polygonal contour.
6. The thrust bearing assembly according to claim 1 , wherein the plurality of valleys and the plurality of peaks are disposed on both the first annular step and the second annular step, which approximate respective polygonal contours in that the respective pluralities of valleys represent respective sides of respective polygons and the respective pluralities of peaks represent respective corners of the respective polygons and the respective pluralities of valleys of both the first annular step and the second annular step are situated in common angular segments.
7. The thrust bearing assembly according to claim 1 , wherein the first race ring is dimensioned to have a component depth measured in an axial direction that corresponds to 0.5 to 1.1 times a first race ring width dimension measured in a radial direction, the width dimension corresponding to 0.15 to 0.3 times an inner diameter of the first race ring.