Bearing assemblies, apparatuses, and related methods of manufacture
View Patent ↗In an embodiment, a bearing assembly may include a support ring to which one or more superhard bearing elements may be mounted. The support ring may include one or more relief features configured to reduce residual stresses in the superhard bearing elements that are induced by brazing the superhard bearing elements to the support ring, operational loads, other processes, or combinations of the foregoing. Reducing the residual stresses in the superhard bearing elements may help prevent damage to the superhard bearing elements. The bearing assembly may be used in subterranean drilling systems and/or other types of systems.
1. A method for manufacturing a radial bearing assembly, the method comprising:
providing a support ring;
forming a plurality of recesses in the support ring that are distributed circumferentially about an axis; and
forming a plurality of relief features in the support ring each of which includes two closed ends that are bounded by the support ring, each of the plurality of relief features disposed between adjacent recesses of the plurality of recesses; and
attaching a plurality of superhard bearing elements to the support ring, with each of the plurality of superhard bearing elements disposed in a corresponding one of the plurality of recesses.
2. The method of claim 1 wherein attaching a plurality of superhard bearing elements to the support ring includes brazing the plurality of superhard bearing elements to the support ring without forming radial cracks in at least one of the plurality of superhard bearing elements.
3. The method of claim 2 wherein brazing the plurality of superhard bearing elements to the support ring includes orienting a superhard bearing surface of the each of the plurality of superhard bearing elements prior to brazing.
4. The method of claim 1 , further comprising:
forming a plurality of second recesses in a second support ring that are distributed circumferentially about an axis; and
forming a plurality of second relief features in the second support ring each of which includes two closed ends that are bounded by the second support ring, each of the plurality of second relief features disposed between adjacent recesses of the plurality of second recesses.
5. The method of claim 4 , further comprising brazing a plurality of second superhard bearing elements to the second support ring.
6. The method of claim 5 , further comprising enclosing the support ring having the plurality of superhard bearing elements attached thereto with the second support ring such that the plurality of superhard bearing elements generally oppose the plurality of second superhard bearing elements of the second support ring.
7. The method of claim 1 wherein at least some of the plurality of relief features are grooves.
8. The method of claim 7 wherein the grooves exhibit a generally semi-cylindrical shape, a generally rectangular shape, a generally crescent shape, a generally diamond shape, or a generally hourglass shape.
9. The method of claim 8 wherein the grooves exhibit substantially the same shape.
10. The method of claim 8 wherein the grooves exhibit different shapes.
11. The method of claim 7 wherein the grooves extend to a maximum depth in the support ring that does not pass completely through a wall of the support ring.
12. The method of claim 11 wherein the maximum depth is about 0.1 inches to about 0.4 inches.
13. The method of claim 7 wherein the grooves extend completely through a wall of the support ring.
14. A method for manufacturing a radial bearing apparatus, the method comprising:
providing a first support ring;
forming a plurality of recesses in the first support ring that are distributed circumferentially about an axis; and
forming a plurality of relief features in the first support ring each of which includes two closed ends that are bounded by the first support ring, each of the plurality of relief features disposed between adjacent recesses of the plurality of recesses in the support ring; and
attaching a plurality of first superhard bearing elements to the first support ring without forming radial cracks in at least one of the plurality of first superhard bearing elements, with each of the plurality of first superhard bearing elements disposed in a corresponding one of the plurality of recesses;
at least partially enclosing the first support ring with a second support ring having a plurality of second superhard bearing elements attached thereto, the plurality of second superhard bearing elements generally opposed to the plurality of first superhard bearing elements.
15. The method of claim 14 , further comprising:
forming a plurality of second recesses in the second support ring that are circumferentially distributed; and
forming a plurality of second relief features in the second support ring each of which includes two closed ends that are bounded by the second support ring, each of the plurality of second relief features disposed between adjacent recesses of the plurality of second recesses.
16. The method of claim 14 wherein at least some of the plurality of relief features are grooves.
17. The method of claim 16 wherein the grooves exhibit substantially the same shape.
18. The method of claim 16 wherein the grooves exhibit substantially different shapes.
19. A method for manufacturing a radial bearing assembly, the method comprising:
providing a support ring;
forming a plurality of recesses in the support ring that are distributed circumferentially about an axis; and
forming a plurality of relief features in the support ring each of which includes two closed ends that are bounded by the support ring, each of the plurality of relief features exhibiting a depth of about 0.1 inches to about 0.4 inch, each of the plurality of relief features disposed between adjacent recesses of the plurality of recesses; and
brazing a plurality of superhard bearing elements to the support ring, with each of the plurality of superhard bearing elements disposed in a corresponding one of the plurality of recesses.
20. The method of claim 19 wherein the depth is about 0.15 inches to about 0.25 inches.