Cutting elements including undulating boundaries between catalyst-containing and catalyst-free regions of polycrystalline superabrasive materials and related earth-boring tools and methods

Patent metadata

Field	Value
Publication number	US-9605488-B2
Application number	US-201414248068-A
Country	US
Kind code	B2
Filing date	Apr 8, 2014
Priority date	Apr 8, 2014
Publication date	Mar 28, 2017
Grant date	Mar 28, 2017

Abstract

Cutting elements for earth-boring tools may include a substrate and a polycrystalline superabrasive material secured to the substrate. The polycrystalline superabrasive material may include a first region including catalyst material in interstitial spaces among interbonded grains of the polycrystalline superabrasive material. A second region at least substantially free of catalyst material in the interstitial spaces among the interbonded grains of the polycrystalline superabrasive material may be located adjacent to the first region. An undulating boundary defined between the first region and the second region may extend from a longitudinal axis of the cutting element to a periphery of the cutting element.

First claim

What is claimed is:

1. A cutting element for an earth-boring tool, comprising:
a substrate; and
a polycrystalline superabrasive material secured to the substrate, the polycrystalline superabrasive material comprising:
a first region including catalyst material in interstitial spaces among interbonded grains of the polycrystalline superabrasive material; and
a second region at least substantially free of catalyst material in the interstitial spaces among the interbonded grains of the polycrystalline superabrasive material, an undulating boundary comprising bumps and dimples formed by crests and troughs of phase-shifted waves extending from a longitudinal axis of the cutting element to a periphery of the cutting element being defined between the first region and the second region.

2. The cutting element of claim 1 , wherein a plane defined by an average height of the undulating boundary with respect to a plane of an interface surface between the substrate and the polycrystalline superabrasive material is at least substantially parallel to the plane of the interface surface.

3. The cutting element of claim 1 , wherein a slope of the undulating boundary at each first point defined by the undulating boundary is different from the slope of the undulating boundary at each adjacent point defined by the undulating boundary, each adjacent point being located about one-fourth of an average wavelength or less from each first point.

4. The cutting element of claim 1 , wherein at least one cross-section of the undulating boundary is sinusoidal.

5. The cutting element of claim 1 , wherein a portion of the polycrystalline superabrasive material in the second region is in a compressive stress state.

6. The cutting element of claim 5 , wherein the portion of the polycrystalline superabrasive material in the compressive stress state is located between peaks of the undulating boundary.

7. The cutting element of claim 1 , wherein the undulating boundary comprises waves exhibiting an average amplitude of between about 40 μm and 50 μm and an average wavelength of between about 100 μm and about 1000 μm.

8. The cutting element of claim 1 , wherein the polycrystalline superabrasive material comprises a concavity proximate the longitudinal axis of the cutting element.

9. An earth-boring tool, comprising:
a body; and
a cutting element secured to the body, the cutting element comprising:
a substrate secured to the body; and
a polycrystalline superabrasive material secured to the substrate, the polycrystalline superabrasive material comprising:
a first region including catalyst material in interstitial spaces among interbonded grains of the polycrystalline superabrasive material; and
a second region at least substantially free of catalyst material in the interstitial spaces among the interbonded grains of the polycrystalline superabrasive material, an undulating boundary comprising bumps and dimples formed by crests and troughs of phase-shifted waves extending from a longitudinal axis of the cutting element to a periphery of the cutting element being defined between the first region and the second region.

10. The earth-boring tool of claim 9 , wherein a plane defined by an average height of the undulating boundary with respect to a plane of an interface surface between the substrate and the polycrystalline superabrasive material is at least substantially parallel to the plane of the interface surface.

11. The earth-boring tool of claim 9 , wherein a slope of the undulating boundary at each first point defined by the undulating boundary is different from the slope of the undulating boundary at each adjacent point defined by the undulating boundary, each adjacent point being located about one-fourth of an average wavelength or less from each first point.

12. The earth-boring tool of claim 9 , wherein at least one cross-section of the undulating boundary is sinusoidal.

13. The earth-boring tool of claim 9 , wherein the undulating boundary comprises waves exhibiting an average amplitude of between about 40 μm and 50 μm and an average wavelength of between about 100 μm and about 1000 μm.

14. The earth-boring tool of claim 9 , wherein the polycrystalline superabrasive material comprises a concavity proximate the longitudinal axis of the cutting element.

15. A method of preparing a cutting element for an earth-boring tool, comprising:
retaining catalyst material within interstitial spaces among interbonded grains in a first region of a polycrystalline superabrasive material, the polycrystalline superabrasive material being secured to a substrate; and
at least substantially completely removing catalyst material from interstitial spaces among interbonded grains in a second region of the polycrystalline superabrasive material, to form an undulating boundary comprising bumps and dimples formed by crests and troughs of phase-shifted waves extending from a longitudinal axis of the cutting element to a periphery of the cutting element between the first region and the second region.

16. The method of claim 15 , wherein at least substantially completely removing catalyst material from the interstitial spaces among the interbonded grains in the second region of the polycrystalline superabrasive material comprises rendering a plane defined by an average height of the undulating boundary with respect to a plane of a surface of the substrate adjacent to the polycrystalline superabrasive material at least substantially parallel to the plane of the surface of the substrate adjacent to the polycrystalline superabrasive material.

17. The method of claim 15 , wherein at least substantially completely removing catalyst material from the interstitial spaces among the interbonded grains in the second region of the polycrystalline superabrasive material comprises rendering at least one cross-section of the undulating boundary sinusoidal.

18. The method of claim 15 , wherein at least substantially completely removing catalyst material from the interstitial spaces among the interbonded grains in the second region of the polycrystalline superabrasive material comprises inducing a compressive residual stress in a portion of the polycrystalline superabrasive material in the second region.

19. The method of claim 15 , wherein at least substantially completely removing catalyst material from the interstitial spaces among the interbonded grains in the second region of the polycrystalline superabrasive material comprises rendering an average amplitude of waves of the undulating boundary to be between about 40 μm and about 50 μm and an average wavelength of the waves of the undulating boundary to be between about 100 μm and about 1000 μm.

20. The method of claim 15 , further comprising forming a concavity in the polycrystalline superabrasive material proximate the longitudinal axis of the cutting element.

Assignees

• Baker Hughes Inc

Inventors

• Stockey David A
• Digiovanni Anthony A

Classifications

• E21B10/5735

  Interface between the substrate and the cutting element · CPC title

• C22C2204/00

  End product comprising different layers, coatings or parts of cermet · CPC title

• C22C29/08

  based on tungsten carbide · CPC title

• C22C26/00

  Alloys containing diamond {or cubic or wurtzitic boron nitride, fullerenes or carbon nanotubes} · CPC title

• B22F2005/005

  Article surface comprising protrusions · CPC title