IP Library Granted Patent US 8,881,361
Granted Patent B1
US 8,881,361 · App. 13/413,100 · Granted Nov 11, 2014

Methods of repairing a rotary drill bit

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Quick Facts
Patent No.
US 8,881,361
App. No.
13/413,100
Granted
Nov 11, 2014
Kind
B1
Abstract

Embodiments of the invention relate to superabrasive compacts including multiple superabrasive cutting portions and methods of repairing a rotary drill bit that employs at least one of such superabrasive compacts.

Claims (54)

1. A method of repairing a rotary drill bit, comprising:

providing the rotary drill bit, the rotary drill bit including a bit body having a plurality of superabrasive cutting elements brazed thereto, at least one of the plurality of superabrasive cutting elements defining a longitudinal axis and including:

a cemented carbide substrate including a first end having a first surface adjacent to a first recess and a second end having a second surface adjacent to a second recess, the first end being spaced from the second end along the longitudinal axis;

a first superabrasive cutting portion bonded at least partially within the first recess of the cemented carbide substrate, the first superabrasive cutting portion including a first working surface facing in a first direction; and

a second superabrasive cutting portion bonded at least partially within the second recess of the cemented carbide substrate and axially spaced from the first superabrasive cutting portion, the second superabrasive cutting portion including a second working surface laterally offset from the first working surface and facing in a second direction that is generally opposite to the first direction;

removing the at least one of the plurality of superabrasive cutting elements from the bit body when the first superabrasive cutting portion is at least partially worn; and

after the act of removing, brazing the at least one of the plurality of superabrasive cutting elements to the bit body with the second superabrasive cutting portion positioned for cutting a subterranean formation during drilling.

2. The method of claim 1 wherein at least one of the first superabrasive cutting portion or the second superabrasive cutting portion comprises a leached region from which a metallic material is at least partially removed.

3. The method of claim 1 wherein at least one of the first or second superabrasive cutting portions comprises a polycrystalline diamond cutting portion integrally formed with the cemented carbide substrate.

4. The method of claim 1 wherein at least one of the first or second superabrasive cutting portions comprises a preformed polycrystalline diamond cutting portion.

5. The method of claim 1 wherein:

the first superabrasive cutting portion comprises at least one first lateral surface and a first cutting edge that generally defines part of a circle, at least a portion of the at least one first lateral surface bonded to the cemented carbide substrate; and

the second superabrasive cutting portion comprises at least one second lateral surface and a second cutting edge that generally defines part of a circle, at least a portion of the at least one second lateral surface bonded to the cemented carbide substrate.

6. The method of claim 1 wherein:

the first surface comprises a top surface and the second surface comprises a bottom surface;

the first superabrasive cutting portion including at least one first lateral surface and a first cutting edge that generally defines part of a circle, wherein at least a portion of the at least one first lateral surface is bonded to the cemented carbide substrate; and

the second superabrasive cutting portion including at least one second lateral surface and a second cutting edge that generally defines part of a circle, wherein at least a portion of the at least one second lateral surface is bonded to the cemented carbide substrate;

the first working surface of the first superabrasive cutting portion and the top surface of the cemented carbide substrate at least partially defining an upper surface of the at least one of the plurality of superabrasive cutting elements; and

the second working surface of the second superabrasive cutting portion and the bottom surface of the cemented carbide substrate at least partially defining a lower surface of the at least one of the plurality of superabrasive cutting elements.

7. The method of claim 1 wherein the cemented carbide substrate comprises:

a first cemented carbide substrate including the first recess; and

a second cemented carbide substrate including the second recess, the second cemented carbide substrate bonded to the first cemented carbide substrate.

8. The method of claim 7 wherein the first cemented carbide substrate is diffusion bonded to the second cemented carbide substrate.

9. The method of claim 7 wherein the first cemented carbide substrate is brazed to the second cemented carbide substrate.

10. The method of claim 1 wherein a superabrasive structure is not disposed on or in at least one peripheral surface of the cemented carbide substrate.

11. The method of claim 1 wherein the first working surface defines a portion of an upper surface of the at least one of the plurality of superabrasive cutting elements, and the second working surface defines a portion of a lower surface of the at least one of the plurality of superabrasive cutting elements.

12. A method of reconstructing a rotary drill bit, comprising:

receiving the rotary drill bit that includes a bit body having a plurality of polycrystalline diamond cutting elements attached thereto, at least one of the plurality of polycrystalline diamond cutting elements brazed within a recess, the at least one of the plurality of polycrystalline diamond cutting elements defining a longitudinal axis and including:

a cemented carbide substrate including a first end having a first surface adjacent to a first recess and a second end having a second surface adjacent to a second recess axially, the first end being spaced from the second end along the longitudinal axis;

a first polycrystalline diamond cutting portion bonded at least partially within the first recess of the cemented carbide substrate, the first polycrystalline diamond cutting portion including a first working surface facing in a first direction; and

a second polycrystalline diamond cutting portion bonded at least partially within the second recess of the cemented carbide substrate and axially spaced from the first polycrystalline diamond cutting portion, the second polycrystalline diamond cutting portion including a second working surface laterally offset from the first working surface and facing in a second direction that is generally opposite to the first direction;

removing the at least one of the plurality of polycrystalline diamond cutting elements from the bit body when the first polycrystalline diamond cutting portion is at least partially worn; and

after the act of removing, brazing the at least one of the plurality of polycrystalline diamond cutting elements within the recess with the second polycrystalline diamond cutting portion positioned for cutting a subterranean formation during drilling.

13. The method of claim 12 wherein at least one of the first or second polycrystalline diamond cutting portions comprises a polycrystalline diamond cutting portion integrally formed with the cemented carbide substrate.

14. The method of claim 12 wherein at least one of the first or second polycrystalline diamond cutting portions comprises a preformed polycrystalline diamond cutting portion.

15. The method of claim 12 wherein:

the first polycrystalline diamond cutting portion comprises at least one first lateral surface and a first cutting edge that generally defines part of a circle, at least a portion of the at least one first lateral surface bonded to the cemented carbide substrate; and

the second polycrystalline diamond cutting portion comprises at least one second lateral surface and a second cutting edge that generally defines part of a circle, at least a portion of the at least one second lateral surface bonded to the cemented carbide substrate.

16. The method of claim 1 wherein at least one of the first polycrystalline diamond cutting portion or the second polycrystalline diamond cutting portion comprises a leached region from which a metallic material is at least partially removed.

17. The method of claim 12 wherein:

the first surface comprises a top surface and the second surface comprises a bottom surface;

the first polycrystalline diamond cutting portion including at least one first lateral surface and a first cutting edge that generally defines part of a circle, wherein at least a portion of the at least one first lateral surface is bonded to the cemented carbide substrate; and

the second polycrystalline diamond cutting portion including at least one second lateral surface and a second cutting edge that generally defines part of a circle, wherein at least a portion of the at least one second lateral surface is bonded to the cemented carbide substrate;

the first working surface of the first polycrystalline diamond cutting portion and the top surface of the cemented carbide substrate at least partially defining an upper surface of the at least one of the plurality of polycrystalline diamond cutting elements; and

the second working surface of the second polycrystalline diamond cutting portion and the bottom surface of the cemented carbide substrate at least partially defining a lower surface of the at least one of the plurality of polycrystalline diamond cutting elements.

18. The method of claim 12 wherein the first working surface defines a portion of an upper surface of the at least one of the plurality of polycrystalline diamond cutting elements, and the second working surface defines a portion of a lower surface of the at least one of the plurality of polycrystalline diamond cutting elements.

19. A method of repairing a subterranean drill system component, comprising:

receiving a rotary drill bit comprising a bit body including a plurality of blades having a plurality of polycrystalline diamond cutting elements brazed thereto, at least one of the plurality of polycrystalline diamond cutting elements defining a longitudinal axis and including:

a substrate including a first end having a first surface adjacent to a first recess and a second end having a second surface adjacent to a second recess that is spaced laterally from the first recess, the first end being spaced from the second end along the longitudinal axis;

a first polycrystalline diamond cutting portion bonded at least partially within the first recess of the substrate, the first polycrystalline diamond cutting portion including a first working surface facing in a first direction and a first cutting edge that generally defines part of a circle; and

a second polycrystalline diamond cutting portion bonded at least partially within the second recess of the substrate and axially spaced from the first polycrystalline diamond cutting portion, the second polycrystalline diamond cutting portion including a second working surface laterally offset from the first working surface and facing in a second direction that is generally opposing the first direction and a second cutting edge that generally defines part of a circle;

removing the at least one of the plurality of polycrystalline diamond cutting elements from the bit body when the first polycrystalline diamond cutting portion is at least partially worn; and

after the act of removing, re-attaching the at least one of the plurality of polycrystalline diamond cutting elements to the bit body with the second polycrystalline diamond cutting portion positioned for cutting a subterranean formation during drilling.

20. The method of claim 19 wherein at least one of the first polycrystalline diamond cutting portion or the second polycrystalline diamond cutting portion comprises a leached region from which a metallic material is at least partially removed.

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 →