Bearing assembly including bearing support ring configured to reduce thermal warping during use
View Patent ↗Various embodiments relate to a bearing assembly including a support ring configured to reduce thermal warping under operational temperature conditions, a bearing apparatus that may utilize such a thrust-bearing assembly, and applications that incorporate the disclosed bearing apparatuses such as downhole motors in subterranean drilling systems, directional drilling systems, and many other apparatuses. In an embodiment, a bearing assembly includes a plurality of superhard bearing elements distributed circumferentially about an axis. The thrust-bearing assembly further includes a support ring having the plurality of superhard bearing elements mounted thereto. The support ring includes at least one thermal-warping-reducing feature configured to reduce a radial moment, compared to if the at least one thermal-warping-reducing feature were absent from the support ring, which is thermally induced in the support ring when the support ring and the plurality of superhard bearing elements are exposed to operational temperature conditions.
1. A bearing assembly, comprising:
a plurality of superhard bearing elements distributed circumferentially about an axis, each of the plurality of superhard bearing elements having a superhard bearing surface, the superhard bearing surfaces are substantially coplanar with each other; and
a support ring having a plurality of recesses, each of the plurality of superhard bearing elements mounted at least partially within a corresponding one of the plurality of recesses, the support ring exhibiting compliance that enables the plurality of superhard bearing elements to remain substantially coplanar with each other at an out-of-plane displacement of 0.00020 inch to about 0.0020 inch when the support ring and the plurality of superhard bearing elements are under operational temperature conditions between 100° C. and 150° C.
2. The bearing assembly of claim 1 wherein the out-of-plane displacement is 0.0005 inch to about 0.0010 inch when the support ring and the plurality of superhard bearing elements are exposed to the operational temperature conditions.
3. The bearing assembly of claim 1 wherein:
each of the plurality of recesses extends inwardly and terminates at a first depth; and
the support ring includes a plurality of radially-extending slots, each of the plurality of radially-extending slots disposed between immediately circumferentially adjacent ones of the plurality of superhard bearing elements, each of the plurality of radially-extending slots extending into the support ring to at least the first depth.
4. The bearing assembly of claim 3 wherein each of the radially-extending slots exhibit a width greater than about 0.0020 inch.
5. The bearing assembly of claim 4 wherein the width is about 0.0020 inch to about 0.100 inch.
6. The bearing assembly of claim 4 wherein the width is about 0.010 inch to about 0.040 inch.
7. The bearing assembly of claim 3 wherein each of the plurality of radially-extending slots is disposed circumferentially about halfway between the immediately adjacent ones of the plurality of superhard bearing elements.
8. The bearing assembly of claim 1 wherein the support ring includes a first support ring portion exhibiting a first thermal expansion coefficient and a second support ring portion joined to the first support ring portion that exhibits a second thermal expansion coefficient that is greater than the first thermal expansion coefficient.
9. The bearing assembly of claim 1 wherein at least a portion of the plurality of superhard bearing elements include a substrate and a polycrystalline diamond table bonded to the substrate.
10. The bearing assembly of claim 1 wherein each of the plurality of superhard bearing elements is brazed, interference-fitted, or fastened to the support ring.
11. The bearing assembly of claim 1 wherein the axis is a thrust axis, and wherein the support ring and the plurality of superhard bearing elements define a thrust-bearing assembly.
12. A bearing assembly, comprising:
a plurality of superhard bearing elements distributed circumferentially about an axis, each of the plurality of superhard bearing elements having a superhard bearing surface, the superhard bearing surfaces lying substantially on the same imaginary surface; and
a support ring, the support ring including:
a first support ring portion exhibiting a first thermal expansion coefficient and a first thickness, the first support ring portion having the plurality of superhard bearing elements mounted thereon; and
a second support ring portion joined to the first support ring portion, the second support ring having a second thickness that is approximately the same as the first thickness and exhibiting a second thermal expansion coefficient that is greater than the first thermal expansion coefficient, the first and second support ring portions collectively configured such that the plurality of superhard bearing elements remain substantially coplanar with each other at an out-of-plane displacement of 0.00020 inch to about 0.0020 inch when the support ring and the plurality of superhard bearing elements are under operational temperature conditions between 100° C. and 150° C.
13. The bearing assembly of claim 12 wherein the out-of-plane displacement is 0.0005 inch to about 0.0010 inch when the support ring and the plurality of superhard bearing elements are exposed to the operational temperature conditions.
14. The bearing assembly of claim 12 wherein the second support ring portion includes at least one of a copper alloy, an aluminum alloy, or brass, and the first support ring portion includes stainless steel or carbon steel.
15. The bearing assembly of claim 12 wherein the first support ring portion and the second support ring portion are brazed together, diffusion bonded together, or mechanically fastened together.
16. The bearing assembly of claim 12 wherein at least a portion of the plurality of superhard bearing elements include a substrate and a polycrystalline diamond table bonded to the substrate.
17. The bearing assembly of claim 12 wherein each of the plurality of superhard bearing elements is brazed, interference-fitted, or fastened to the support ring.
18. The bearing assembly of claim 12 wherein the axis is a thrust axis, and wherein the support ring and the plurality of superhard bearing elements define a thrust-bearing assembly.
19. A bearing assembly, comprising:
a plurality of superhard bearing elements distributed circumferentially about an axis, each of the plurality of superhard bearing elements including a superhard bearing surface, the superhard bearing surfaces of the plurality of superhard bearing elements lying substantially on the same imaginary surface; and
a support ring having a plurality of recesses each extending inwardly and terminating at a first depth, each of the plurality of superhard bearing elements mounted at least partially within a corresponding one of the plurality of recesses, the support ring including:
a plurality of slots formed in the support ring, each of the plurality of slots disposed between immediately circumferentially adjacent ones of the plurality of superhard bearing elements, each of the plurality of slots extending into the support ring to at least the first depth, the plurality of slots increasing compliance of the support ring during use compared to if the plurality of slots were not present in the support ring.
20. The bearing assembly of claim 19 wherein the imaginary surface is a plane, the axis is a thrust axis, and each of the plurality of slots are radially extending.
21. The bearing assembly of claim 19 wherein each of the plurality of slots is disposed circumferentially between a respective pair of immediately circumferentially adjacent ones of the plurality of superhard bearing elements.
22. The bearing assembly of claim 19 wherein each of the plurality of slots exhibit a width greater than about 0.0020 inch.
23. The bearing assembly of claim 22 wherein the width is about 0.0020 inch to about 0.100 inch.
24. The bearing assembly of claim 22 wherein the width is about 0.010 inch to about 0.040 inch.