Methods of operating bearing apparatuses
View Patent ↗In an embodiment, a bearing apparatus comprises a first bearing assembly including a plurality of circumferentially-spaced first bearing elements each of which includes a first bearing surface. The bearing apparatus further includes a second bearing assembly including a plurality of circumferentially-spaced second bearing elements each of which includes a second bearing surface oriented to engage the first bearing surfaces of the first bearing assembly during operation. At least one of the second bearing elements may be circumferentially spaced from an adjacent one of the second bearing elements by a lateral spacing greater than a lateral dimension of the at least one of the second bearing elements.
1. A method of operating a thrust-bearing apparatus, comprising:
providing the thrust-bearing apparatus, wherein the thrust-bearing apparatus includes:
a first bearing assembly including a plurality of circumferentially-spaced first bearing elements each of which includes a first bearing surface including polycrystalline diamond, each of the plurality of circumferentially-spaced first bearing elements circumferentially spaced from a circumferentially nearest one of the plurality of circumferentially-spaced first bearing elements by a respective first lateral spacing less than a respective first lateral dimension of the circumferentially nearest one of the plurality of circumferentially-spaced first bearing elements; and
a second bearing assembly including a plurality of circumferentially-spaced second bearing elements each of which includes a second bearing surface oriented to engage the first bearing surfaces of the first bearing assembly during operation, each of the plurality of circumferentially-spaced second bearing elements circumferentially spaced from a circumferentially nearest one of the plurality of circumferentially-spaced second bearing elements by a respective second lateral spacing greater than a respective second lateral dimension of the circumferentially nearest one of the plurality of circumferentially-spaced second bearing elements, wherein the respective second lateral spacing is greater than the respective first lateral spacing, and wherein the respective second lateral dimension is equal to or greater than the respective first lateral spacing; and
rotating one of the first bearing assembly or the second bearing assembly.
2. The method of claim 1 wherein the number of the second bearing elements is less than the number of the first bearing elements, and wherein at least some of the plurality of circumferentially-spaced second bearing elements are more thermally stable than the plurality of circumferentially-spaced first bearing elements.
3. The method of claim 1 wherein the respective second lateral spacing is at least about two times greater than an average of the second lateral dimensions of the plurality of circumferentially-spaced second bearing elements.
4. The method of claim 1 wherein the plurality of circumferentially-spaced second bearing elements are substantially equally circumferentially spaced from each other.
5. The method of claim 1 wherein the respective first lateral spacing is less than an average of the first lateral dimensions exhibited by the plurality of circumferentially-spaced first bearing elements.
6. The method of claim 1 wherein the second bearing assembly includes a bearing support including the plurality of circumferentially-spaced second bearing elements mounted thereto, the bearing support including at least one flow obstruction element positioned and configured to provide a selected fluid flow over the second bearing surfaces of the plurality of circumferentially-spaced second bearing elements.
7. The method of claim 1 wherein each of the plurality of circumferentially-spaced first bearing elements includes a substrate having a polycrystalline diamond table defining the first bearing surface comprising the polycrystalline diamond.
8. The method of claim 1 wherein each of the plurality of circumferentially-spaced second bearing elements includes a substrate having a polycrystalline diamond table defining the second bearing surface.
9. The method of claim 1 wherein one of the first or second thrust-bearing assemblies is a stator and the other one of the first or second thrust-bearing assemblies is a rotor.
10. A method of operating a thrust-bearing apparatus, comprising:
providing the thrust-bearing apparatus, wherein the thrust-bearing apparatus includes:
a first bearing assembly including a plurality of circumferentially-spaced first bearing elements each of which includes a first polycrystalline diamond body defining a first bearing surface, each of the plurality of circumferentially-spaced first bearing elements circumferentially spaced from a circumferentially nearest one of the plurality of circumferentially-spaced first bearing elements by a respective first lateral spacing less than a respective first lateral dimension of the circumferentially nearest one of the plurality of circumferentially-spaced first bearing elements; and
a second bearing assembly including a plurality of circumferentially-spaced second bearing elements each of which includes a second polycrystalline diamond body defining a second bearing surface oriented to engage the first bearing surfaces of the first bearing assembly during operation, each of the plurality of circumferentially-spaced second bearing elements circumferentially spaced from a circumferentially nearest one of the plurality of circumferentially-spaced second bearing elements by a respective second lateral spacing greater than a respective second lateral dimension of the circumferentially nearest one of the plurality of circumferentially-spaced second bearing elements, wherein the respective second lateral spacing is greater than the respective first lateral spacing, and wherein the respective second lateral dimension is equal to or greater than the respective first lateral spacing; and
rotating one of the first bearing assembly or the second bearing assembly.
11. The method of claim 10 wherein the number of the second bearing elements is less than the number of the first bearing elements, and wherein at least some of the plurality of circumferentially-spaced second bearing elements are more thermally stable than the plurality of circumferentially-spaced first bearing elements.
12. The method of claim 10 wherein the respective second lateral spacing is at least about two times greater than an average of the second lateral dimensions of the plurality of circumferentially-spaced second bearing elements.
13. The method of claim 10 wherein the plurality of circumferentially-spaced second bearing elements are substantially equally circumferentially spaced from each other.
14. The method of claim 10 wherein the respective first lateral spacing is less than an average of the first lateral dimensions exhibited by the plurality of circumferentially-spaced first bearing elements.
15. The bearing apparatus of claim 10 wherein the second bearing assembly includes a bearing support including the plurality of circumferentially-spaced second bearing elements mounted thereto, the bearing support including at least one flow obstruction element positioned and configured to provide a selected fluid flow over the second bearing surfaces of the plurality of circumferentially-spaced second bearing elements.
16. The method of claim 10 wherein each of the plurality of circumferentially-spaced first bearing elements includes a substrate having a polycrystalline diamond table comprising the first polycrystalline diamond body.
17. The method of claim 10 wherein each of the plurality of circumferentially-spaced second bearing elements includes a substrate having a polycrystalline diamond table comprising the second polycrystalline diamond body.
18. The method of claim 11 wherein one of the first or second thrust-bearing assemblies is a stator and the other one of the first or second thrust-bearing assemblies is a rotor.
19. A method of operating a thrust-bearing apparatus, comprising:
providing the thrust-bearing apparatus, wherein the thrust-bearing apparatus includes:
a stator including a plurality of circumferentially-spaced first bearing elements each of which includes a first polycrystalline diamond body defining a first bearing surface, each of the plurality of circumferentially-spaced first bearing elements circumferentially spaced from a circumferentially nearest one of the plurality of circumferentially-spaced first bearing elements by a respective first lateral spacing less than a respective first lateral dimension of the circumferentially nearest one of the plurality of circumferentially-spaced first bearing elements; and
a rotor including a plurality of circumferentially-spaced second bearing elements each of which includes a second polycrystalline diamond body defining a second bearing surface oriented to engage the first bearing surfaces of the first bearing assembly during operation, each of the plurality of circumferentially-spaced second bearing elements circumferentially spaced from a circumferentially nearest one of the plurality of circumferentially-spaced second bearing elements by a respective second lateral spacing greater than a respective second lateral dimension of the circumferentially nearest one of the plurality of circumferentially-spaced second bearing elements, wherein the respective second lateral spacing is greater than the respective first lateral spacing, and wherein the respective second lateral dimension is equal to or greater than the respective first lateral spacing;
wherein the number of the second bearing elements is less than the number of the first bearing elements, and wherein at least some of the plurality of circumferentially-spaced second bearing elements are more thermally stable than the plurality of circumferentially-spaced first bearing elements; and
rotating the rotor relative to the stator.