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US5061293A Expired / Lapsed US ⏱️ 0.0 years remaining

Cutting elements for rotary drill bits

Assignee: Individual
•
Filing: 1990-05-14
•
Granted: 1991-10-29
•
Expires: 2010-05-14
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Abstract

Abstract A preform cutting element for a rotary drill bit includes a layer of polycrystalline diamond material, the rear face of which is bonded to the front face of a backing layer of less hard material, such as tungsten carbide. The rear face of the backing layer is substantially greater in area than the rear face of the diamond layer. A method of manufacturing such cutting elements comprises forming an intermediate structure comprising polycrystalline diamond material bonded between two outer layers of tungsten carbide, and then cutting the intermediate structure to provide two pieces, each of the pieces including part of the diamond material and at least a major part of a respective one of the two outer layers.

Inventors

  • 👤 John D. Barr
  • 👤 Thomas A. Newton, Jr.

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-06 05:22
CPC Classifications
E; E21; E21B; E21B10/00; E21B10/46; E21B10/56; E21B10/567; B; B23; B23P; B23P15/00; B23P15/28

Claims Analysis

Total Claims: 8
Claim 1
Independent Claim 84 words
A method of manufacturing preform cutting elements comprising the steps of forming, in a high pressure, high temperature press, an intermediate structure comprising superhard material bonded between two outer layers of less hard material, the outer layers providing opposed outer faces respectively of the intermediate structure, and then cutting the intermediate structure to provide at least two pieces, each of said two pieces including part of the superhard material and at least a major part of a respective one of the two outer layers.
Claim 2
Independent Claim 84 words
A method of manufacturing preform cutting elements comprising the steps of forming, in a high pressure, high temperature press, an intermediate structure comprising superhard material bonded between two outer layers of less hard material, the outer layers providing opposed outer faces respectively of the intermediate structure, and then cutting the intermediate structure to provide at least two pieces, each of said two pieces including part of the superhard material and at least a major part of a respective one of the two outer layers.
Claim 3
Dependent Claim 22 words
A method according to claim 1, wherein the intermediate structure is cut substantially symmetrically so that the two pieces are substantially similar.
Claim 4
Dependent Claim 61 words
A method according to claim 1, wherein the superhard material is in the form of a single layer of material, the intermediate structure being divided into said two pieces by a cut at least a portion of which has a component extending in the direction of the thickness of the intermediate structure so as to divide the superhard layer into two.
Claim 5
Dependent Claim 58 words
A method according to claim 3, wherein the intermediate structure is divided into said two pieces by a cut having a first part substantially parallel to one face of the superhard layer, a second part which passes transversely through the superhard layer, and a third part which is substantially parallel to the other face of the superhard layer.
Claim 6
Dependent Claim 26 words
A method according to claim 4, wherein said first and third parts of the cut are spaced from the adjacent faces of the superhard layer respectively.
Claim 7
Dependent Claim 25 words
A method according to claim 4, wherein said first and third parts of the cut extend along the adjacent faces of the superhard layer respectively.
Claim 8
Dependent Claim 72 words
A method according to claim 1, wherein the superhard material is in the form of at least two layers of material which are spaced apart in the direction of the thickness of the intermediate structure, the intermediate structure being divided into said two pieces by a cut at least a portion of which has a component extending transversely to the thickness of the intermediate structure and between said layers of superhard material.

References Cited (Backward Citations)

US4219339A Cited
US4225322A Cited
US4255165A Cited
US4259090A Cited
US4539018A Cited
US4694918A Cited
US4995887A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1994-10-28 1995-04-29 1995-10-29 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1998-10-28 1999-04-29 1999-10-29 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2002-10-28 2003-04-29 2003-10-29 $7700.00 Window Closed / Lapsed

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