Polycrystalline diamond compact
US-12044075-B2 · Jul 23, 2024 · US
US9664237B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9664237-B2 |
| Application number | US-201414529896-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 31, 2014 |
| Priority date | Oct 31, 2014 |
| Publication date | May 30, 2017 |
| Grant date | May 30, 2017 |
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Official abstract text for this publication.
A universal joint assembly includes a hollow upper shaft, a lower shaft extending at least partially within the upper shaft, and a cage having a plurality of bearing apertures. Each bearing aperture includes a pair of opposed loading pads having a distinct inner wall surface sector extending radially inward into the at least one bearing aperture. The cage receives at least a portion of the lower shaft and is positioned within the hollow upper shaft. The assembly further includes at least one upper tilt pin extending through the upper shaft and a bearing aperture of the plurality of bearing apertures, and a lower tilt pin extending through the lower shaft and a bearing aperture of the plurality of bearing apertures.
Opening claim text (preview).
Having thus described the invention, it is claimed: 1. A cardan joint cage comprising: a rotatable cardan joint cage, the cardan joint cage configured to rotatably couple a first shaft and a second shaft of a universal joint assembly having a spin axis; a first opposed pair of bearing apertures disposed in the cage about a first axis perpendicular to the spin axis; a second opposed pair of bearing apertures disposed in the cage about a second axis perpendicular to the spin axis, the first axis and the second axis perpendicular to one another; and each of the bearing apertures having an inner wall surface and a pair of opposed loading pads extending radially inward into the at least one bearing aperture, the opposed loading pads oriented along a predetermined load path in a transverse plane of the cage that is transverse relative to the spin axis. 2. The cardan joint cage of claim 1 , wherein the opposed loading pads are discontiguous along the inner wall surface. 3. The cardan joint cage of claim 1 , wherein each loading pad of the pair of opposed loading pads is a non-adjoining sector of a circumference of the at least one bearing aperture, the sector defining a portion of the circumference having a sector radial angle. 4. The cardan joint cage of claim 3 , wherein the sector radial angle is between 15° and 120°. 5. The cardan joint cage of claim 3 , wherein the sector radial angle is between 75° and 105°. 6. The cardan joint cage of claim 3 , wherein the sector radial angle is approximately 90°. 7. The cardan joint cage of claim 1 , wherein the opposed loading pads have a loading pad size corresponding to the predetermined load path. 8. A universal joint assembly comprising: a hollow upper shaft; a lower shaft extending at least partially within the upper shaft; a rotatable joint cage having a plurality of bearing apertures comprising a first opposed pair of bearing apertures disposed in the cage about a first axis perpendicular to a spin axis of the assembly and a second opposed pair of bearing apertures disposed in the cage about a second axis perpendicular to the spin axis, the first axis and the second axis perpendicular to one another, each bearing aperture having a pair of opposed loading pads having a distinct inner wall surface sector extending radially inward into the at least one bearing aperture, the opposed loading pads oriented along a predetermined load path in a transverse plane of the cage that is transverse relative to the spin axis, the cage receiving at least a portion of the lower shaft, the cage positioned within the hollow upper shaft; at least one upper tilt pin extending through the upper shaft and the first opposed pair of bearing apertures; and a lower tilt pin extending through the lower shaft and the second opposed pair of bearing apertures. 9. The assembly of claim 8 , wherein the inner wall surface of each bearing aperture includes sectors that are discontiguous with the inner wall surface of opposed loading pads. 10. The assembly of claim 8 , wherein each loading pad of the opposed loading pads is a sector of a circumference of its respective bearing aperture, the sector defining a portion of the circumference having a sector radial angle. 11. The assembly of claim 10 , wherein the sector radial angle is between 60° and 120°. 12. The assembly of claim 10 , wherein the sector radial angle is between 75° and 105°. 13. The assembly of claim 10 , wherein the sector radial angle is approximately 90°. 14. The assembly of claim 8 , wherein the opposed loading pads have a loading pad size corresponding to the predetermined load path. 15. A method of fabricating a rotatable cardan joint cage, the method comprising: forming the rotatable cardan joint cage, the cardan joint cage configured to rotatably couple a first shaft and a second shaft of a universal joint assembly having a spin axis with a first opposed pair of bearing apertures disposed in the cage about a first axis perpendicular to the spin axis and a second opposed pair of bearing apertures disposed in the cage about a second axis perpendicular to the spin axis, the first axis and the second axis perpendicular to one another; and removing material from a portion of the circumference of each bearing aperture to define a pair of opposed loading pads extending radially inward into each aperture, the opposed loading pads oriented along a predetermined load path in a transverse plane of the cage that is transverse relative to the spin axis. 16. The method of claim 15 , wherein the step of removing material further comprises removing material from an area that is unloaded by a load path in a transverse plane of the cage. 17. The method of claim 15 , further comprising defining each loading pad as a sector of the circumference of the at least one bearing aperture, the sector defining a portion of the circumference having a sector radial angle that defines a loading pad size. 18. The method of claim 17 , further comprising forming the sector radial angle between 15° and 120°. 19. The method of claim 17 , further comprising forming the sector radial angle between 75° and 105°. 20. The method of claim 17 , further comprising forming the sector radial angle as approximately 90°.
Followed by cutting or removing material · CPC title
Making specific metal objects by operations not covered by a single other subclass or a group in this subclass · CPC title
bearings (see also F16C33/00) · CPC title
Joints, e.g. ball joints, universal joints · CPC title
Couplings · CPC title
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