IP Library Granted Patent US 8,616,770
Granted Patent B2
US 8,616,770 · App. 13/599,752 · Granted Dec 31, 2013

Bearing apparatuses, systems including same, and related methods

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Quick Facts
Patent No.
US 8,616,770
App. No.
13/599,752
Granted
Dec 31, 2013
Kind
B2
Abstract

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.

Claims (39)

1. A bearing apparatus, comprising:

a first bearing assembly including a plurality of circumferentially-spaced first bearing elements each of which includes 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; and

a bearing support ring having the plurality of circumferentially-spaced second bearing elements mounted thereto;

wherein each of the plurality of circumferentially-spaced second bearing elements includes a second bearing surface oriented to engage the first bearing surfaces of the first bearing assembly during operation;

wherein each of the plurality of circumferentially-spaced second bearing elements is 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, the second lateral spacing greater than the first lateral spacing; and

wherein the bearing support includes 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, the at least one flow obstruction element is positioned circumferentially between circumferentially adjacent second bearing elements of the plurality of circumferentially-spaced second bearing elements and comprises a terminal surface positioned below each of the second bearing surfaces.

2. The bearing apparatus 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.

3. The bearing apparatus of claim 1 wherein the plurality of circumferentially-spaced second bearing elements are substantially equally circumferentially spaced from each other.

4. The bearing apparatus 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.

5. The bearing apparatus of claim 1 wherein the at least one flow obstruction element is laterally spaced a distance from a circumferentially adjacent second bearing element of the plurality of circumferentially-spaced second bearing elements less than an average lateral dimension of the plurality of circumferentially-spaced second bearing elements.

6. The bearing apparatus of claim 1 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.

7. The bearing apparatus of claim 1 wherein the number of the second bearing elements is less than the number of the first bearing elements.

8. The bearing apparatus of claim 1 wherein the first bearing assembly comprises a first bearing support including the plurality of circumferentially-spaced first bearing elements mounted thereto.

9. The bearing apparatus of claim 1 wherein the plurality of circumferentially-spaced first bearing elements and the plurality of circumferentially-spaced second bearing elements are distributed about a thrust axis.

10. The bearing apparatus of claim 1 wherein the first bearing surfaces of the plurality of circumferentially-spaced first bearing elements and the second bearing surfaces of the plurality of circumferentially-spaced second bearing elements are generally radially oriented.

11. The bearing apparatus of claim 1 wherein each of the first and second bearing surfaces comprises polycrystalline diamond.

12. A bearing apparatus, comprising:

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.

13. The bearing apparatus of claim 12 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.

14. The bearing apparatus of claim 12 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.

15. The bearing apparatus of claim 12 wherein the plurality of circumferentially-spaced second bearing elements are substantially equally circumferentially spaced from each other.

16. The bearing apparatus of claim 12 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.

17. The bearing apparatus of claim 12 wherein the second bearing assembly comprises 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.

18. The bearing apparatus of claim 12 wherein each of the second bearing surfaces comprises polycrystalline diamond.

19. A motor assembly for use in a drilling system, the motor assembly comprising:

a motor operable to apply torque to a rotary drill bit, the motor operably coupled to a bearing apparatus, the bearing apparatus including:

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.

20. The motor assembly of claim 19 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.

21. The motor assembly of claim 19 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.

22. The motor assembly of claim 19 wherein the plurality of circumferentially-spaced second bearing elements are substantially equally circumferentially spaced from each other.

23. The motor assembly of claim 19 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.

24. The motor assembly of claim 19 wherein the second bearing assembly comprises 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.

25. The motor assembly of claim 19 wherein each of the second bearing surfaces comprises polycrystalline diamond.

Assignments (5)
SECURITY INTEREST Recorded Jul 18, 2025
From: US SYNTHETIC CORPORATION
To: KEYBANK NATIONAL ASSOCIATION
Reel/Frame 074973/0089 →
RELEASE OF SECURITY INTEREST IN PATENTS Recorded Jul 17, 2025
From: JPMORGAN CHASE BANK, N.A.
To: CHAMPIONX LLC; APERGY ESP SYSTEMS, LLC; APERGY BMCS ACQUISITION CORP; HARBISON-FISCHER, INC.; NORRIS RODS, INC.,; NORRIS RODS, INC.,; NORRISEAL-WELLMARK, INC.; PCS FERGUSON, INC.; QUARTZDYNE, INC.; US SYNTHETIC CORPORATION
Reel/Frame 072004/0019 →
RELEASE OF SECURITY INTEREST Recorded Jun 7, 2022
From: BANK OF AMERICA, N.A.
To: ACE DOWNHOLE, LLC; HARBISON-FISCHER, INC.; NORRIS RODS, INC.; PCS FERGUSON, INC.; QUARTZDYNE, INC.; SPIRIT GLOBAL ENERGY SOLUTIONS, INC.; THETA OILFIELD SERVICES, INC.; APERGY BMCS ACQUISITION CORP.; NORRISEAL-WELLMARK, INC.; US SYNTHETIC CORPORATION; WINDROCK, INC.
Reel/Frame 060305/0001 →
SECURITY INTEREST Recorded Jun 5, 2020
From: ACE DOWNHOLE, LLC; APERGY BMCS ACQUISITION CORP.; HARBISON-FISCHER, INC.; NORRIS RODS, INC.; NORRISEAL-WELLMARK, INC.; PCS FERGUSON, INC.; QUARTZDYNE, INC.; SPIRIT GLOBAL ENERGY SOLUTIONS, INC.; THETA OILFIELD SERVICES, INC.; US SYNTHETIC CORPORATION; WINDROCK, INC.
To: BANK OF AMERICA, N.A.
Reel/Frame 053790/0001 →
SECURITY AGREEMENT Recorded May 9, 2018
From: APERGY (DELAWARE) FORMATION, INC.; APERGY BMCS ACQUISITION CORP.; APERGY ENERGY AUTOMATION, LLC; HARBISON-FISCHER, INC.; NORRISEAL-WELLMARK, INC.; PCS FERGUSON, INC.; QUARTZDYNE, INC.; SPIRIT GLOBAL ENERGY SOLUTIONS, INC.; US SYNTHETIC CORPORATION; WINDROCK, INC.
To: JPMORGAN CHASE BANK, N.A.
Reel/Frame 046117/0015 →