IP Library Granted Patent US 10,173,300
Granted Patent B1
US 10,173,300 · App. 14/876,159 · Granted Jan 8, 2019

Polycrystalline diamond compact, drill bit incorporating same, and methods of manufacture

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Quick Facts
Patent No.
US 10,173,300
App. No.
14/876,159
Granted
Jan 8, 2019
Kind
B1
Abstract

Methods of making superabrasive elements may include forming a first superabrasive body, forming discrete components from the first superabrasive body, and then forming a second abrasive element from the discrete components. For example, microstructures (e.g., micro-cylinders or other geometries) may be formed from the first superabrasive element, catalyst materials may be removed from the microstructures, with the microstructures being recombined and bonded during a subsequent high-pressure, high-temperature (HPHT) process. In other embodiments, superabrasive elements may be formed to include microfeatures formed in a surface of a superabrasive body or table. For example, blind holes or slots may be formed in a surface of the element for use in attaching the superabrasive table to a substrate. The holes may be coated to provide an impermeable surface, or they may be filled with a metallic material to enhance the attachment to a substrate.

Claims (46)

1. A method of forming a superabrasive element, the method comprising:

forming a first superabrasive body comprising a polycrystalline table in a high-pressure, high-temperature (HPHT) process, wherein forming the first superabrasive body includes sweeping a catalyst material into a plurality of diamond grains during the HPHT process, removing the catalyst material from interstitial spaces between bonded diamond grains subsequent to the HPHT process;

forming a plurality of discrete micro-structures from the superabrasive body;

forming a second superabrasive body from at least some of the plurality of discrete structures in an HPHT process;

forming a material coating on the at least some of the plurality of micro-structures subsequent to removing catalyst material and prior to forming the second superabrasive body.

2. The method according to claim 1 , wherein forming a plurality of micro-structures includes forming at least one of a cylinder, a sphere, a polyhedron, a disc and a platelet.

3. The method according to claim 1 , further comprising forming the plurality of micro-structures by an electric discharge machining (EDM) process.

4. The method according to claim 1 , further comprising maintaining the at least some of the plurality of micro-structures free of catalyst material during the HPHT process associated with forming the second superabrasive body.

5. The method according to claim 4 , further comprising attaching the second superabrasive body to a substrate.

6. The method according to claim 5 , further comprising forming a plurality of micro-features in a surface of the second superabrasive body that is to be bonded to the substrate.

7. The method according to claim 6 , wherein forming a plurality of micro-features includes forming a plurality of blind holes.

8. The method according to claim 7 , further comprising disposing a material in the plurality of blind holes prior to attaching the superabrasive body to the substrate.

9. A superabrasive element comprising:

a superabrasive body comprising a plurality of pre-formed, superabrasive microstructures, the microstructures being bonded to one another through a high-pressure, high-temperature (HPHT) process;

wherein a plurality of interstitial spaces between the plurality of bonded microstructures include a catalyst material disposed therein and wherein a plurality of interstitial spaces within each of the microstructures are substantially devoid of any catalyst material;

wherein each of the plurality of microstructures has a material coating at least partially thereon.

10. A superabrasive element comprising:

a superabrasive body comprising a plurality of pre-formed, micro-cut, superabrasive microstructures, the microstructures being bonded to one another through a high-pressure, high-temperature (HPHT) process;

wherein a plurality of interstitial spaces between the plurality of bonded microstructures include a catalyst material disposed therein and wherein a plurality of interstitial spaces within each of the microstructures are substantially devoid of any catalyst material;

wherein the superabrasive element further comprises a plurality of diamond grains intermixed with and bonded to the plurality of plurality of microstructures.

11. The superabrasive element of claim 10 , wherein the plurality of pre-formed, micro-cut, superabrasive microstructures, includes a plurality of pre-formed, laser-cut superabrasive microstructures are leached subsequent to being laser-cut.

12. The superabrasive element of claim 11 , wherein the plurality of pre-formed, laser-cut, superabrasive microstructures.

13. The superabrasive element of claim 10 , wherein the superabrasive body exhibits a coercivity of about 115 Oersteds or more.

14. The superabrasive element of claim 10 , wherein the superabrasive body exhibits a specific magnetic saturation of about 15 Gauss·cm 3 /grams or less.

15. A superabrasive element comprising:

a superabrasive body bonded to a preformed, superabrasive ring, wherein the superabrasive body includes a plurality of interstitial spaces having a catalyst material disposed therein, and wherein the superabrasive ring includes a plurality of interstitial spaces being substantially devoid of any catalyst material.

16. The superabrasive element of claim 15 , wherein the superabrasive body comprises polycrystalline diamond, and wherein the preformed superabrasive ring comprises polycrystalline diamond.

17. The superabrasive element of claim 16 , further comprising a material coating on the superabrasive ring.

18. A rotary drill bit for drilling a subterranean formation, the drill bit comprising:

a shank;

a bit body attached to the shank;

at least one superabrasive element coupled with the bit body, the at least one superabrasive element comprising:

a superabrasive body comprising a plurality of pre-formed, superabrasive microstructures, the microstructures being bonded to one another through a high-pressure, high-temperature (HPHT) process;

wherein a plurality of interstitial spaces between the plurality of bonded microstructures include a catalyst material disposed therein and wherein a plurality of interstitial spaces within each of the microstructures are substantially devoid of any catalyst material;

wherein each of the plurality of microstructures has a material coating at least partially thereon.

19. A rotary drill bit for drilling a subterranean formation, the drill bit comprising:

a shank;

a bit body attached to the shank;

at least one cutting element coupled with the bit body, the at least one cutting element comprising:

a superabrasive body bonded to a preformed, superabrasive ring, wherein the superabrasive body includes a plurality of interstitial spaces having a catalyst material disposed therein, and wherein the superabrasive ring includes a plurality of interstitial spaces being substantially devoid of any catalyst material.

20. A rotary drill bit for drilling a subterranean formation, the drill bit comprising:

a shank;

a bit body attached to the shank;

at least one superabrasive element coupled with the bit body, the at least one superabrasive element comprising a superabrasive body, the superabrasive body comprising a plurality of pre-formed, superabrasive microstructures, the microstructures being bonded to one another through a high-pressure, high-temperature (HPHT) process;

wherein a plurality of interstitial spaces between the plurality of bonded microstructures include a catalyst material disposed therein and wherein a plurality of interstitial spaces within each of the microstructures are substantially devoid of any catalyst material;

wherein the superabrasive element further comprises a plurality of diamond grains intermixed with and bonded to the plurality of plurality of microstructures.

Assignments (5)
SECURITY INTEREST Recorded Jul 18, 2025
From: US SYNTHETIC CORPORATION
To: KEYBANK NATIONAL ASSOCIATION
Reel/Frame 074973/0089 →
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 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 6, 2015
From: MIESS, DAVID P.
To: US SYNTHETIC CORPORATION
Reel/Frame 036738/0187 →