IP Library Granted Patent US 10,730,164
Granted Patent B2
US 10,730,164 · App. 15/849,270 · Granted Aug 4, 2020

Process of forming an abrasive article

Inventors: Ji Xiao (Shanghai, CN); Aiyun Luo (Shanghai, CN); Ignazio Gosamo (Léglise, BE); Vivian Susek (Metz, FR)
Assignee: SAINT-GOBAIN ABRASIVES, INC/SAINT-GOBAIN ABRASIFS
B24D3/06B24D5/06B24D5/123B24D7/06B24D18/0009
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Quick Facts
Patent No.
US 10,730,164
App. No.
15/849,270
Granted
Aug 4, 2020
Kind
B2
Abstract

A process can include forming at least one precursor abrasive component on a core and infiltrating at least a portion of the precursor abrasive component. The precursor abrasive component can include a body including a metal bond matrix and abrasive particles. Infiltrating can be performed after forming the precursor abrasive component with an infiltrant material. The infiltrant material can include a metal element, an alloy or a combination thereof. In an embodiment, forming at least one precursor abrasive component can include simultaneously joining the precursor abrasive component to the core.

Claims (31)

1. A process, comprising:

forming at least one precursor abrasive component on a core, the precursor abrasive component including a body having a metal bond matrix and abrasive particles contained within the metal bond matrix, wherein the body of the precursor abrasive component comprises:

a porosity of at least 10% and at most 50 vol % for a total volume of the body

a content of the abrasive particles of at least 2 vol % and at most 50 vol % for the total volume of the body; and

a content of the metal bond matrix of at least 20 vol % and at most 60 vol % for the total volume of the body; and

infiltrating at least a portion of the body after forming,

wherein forming the at least one precursor abrasive component on the core comprises simultaneous formation of the body of the at least one precursor abrasive component and joining of the at least one precursor abrasive component to the core.

2. The process of claim 1 , wherein forming the precursor abrasive component on the core comprises simultaneous formation of bodies of a plurality of precursor abrasive components and joining of the plurality of precursor abrasive components directly to the core.

3. The process of claim 1 , wherein infiltrating comprises applying an infiltrant material to at least a portion of the body, a portion of the core, or a portion of both.

4. The process of claim 3 , wherein the infiltrant material comprises a metal element, a metal alloy, or a combination thereof.

5. The process of claim 3 , further comprising heating at least a portion of the at least one precursor component.

6. The process of claim 5 , wherein heating is performed at a temperature of at least a melting temperature of the infiltrant material.

7. The process of claim 1 , wherein forming at least one precursor abrasive component on the core comprises applying a pressure to a mixture including a metal bond material and the abrasive particles.

8. The process of claim 2 , wherein forming at least one precursor abrasive component on the core comprises a single pressing operation.

9. The process of claim 1 , wherein the abrasive particles comprise a superabrasive including diamond, cubic boron nitride, or any combination thereof.

10. The process of claim 1 , further comprising forming at least one abrasive component on the core.

11. A process, comprising:

forming at least one precursor abrasive component on a core, the precursor abrasive component including a body having a metal bond matrix and abrasive particles contained within the metal bond matrix, wherein forming the at least one precursor abrasive component on the core comprises simultaneous formation of the body of the at least one precursor abrasive component and joining of the precursor abrasive component to the core, wherein the body of the precursor abrasive component comprises:

a porosity of at least 10% and at most 50 vol % for a total volume of the body

a content of the abrasive particles of at least 2 vol % and at most 50 vol % for the total volume of the body; and

a content of the metal bond matrix of at least 20 vol % and at most 60 vol % for the total volume of the body;

forming at least one infiltrant portion including an infiltrant material while forming the at least one precursor abrasive component; and

heating the at least one precursor abrasive segment and the at least one infiltrant portion to infiltrate the precursor abrasive component with the infiltrant material and forming at least one abrasive component on the core.

12. The process of claim 11 , wherein forming the precursor abrasive component on the core comprises simultaneous formation of bodies of a plurality of precursor abrasive components and joining of the plurality of precursor abrasive components to the core.

13. The process of claim 11 , wherein the infiltrant material comprises a transition metal element, an alloy including a transition metal element, or a combination thereof.

14. The process of claim 11 , wherein heating is performed at a temperature of at least a melting temperature of the infiltrant material.

15. The process of claim 12 , wherein forming at least one precursor abrasive component on the core comprises a single pressing operation.

16. The process of claim 11 , wherein forming at least one precursor abrasive component on the core comprises cold pressing.

17. The process of claim 15 , wherein pressing is performed at a pressure in a range including at least 100 MPa and at most 3000 MPa.

18. The process of claim 11 , wherein the abrasive component comprises a content of the infiltrant material of at least 10 wt. % and at most 45 wt. % for a total weight of the abrasive component.

19. The process of claim 11 , wherein the abrasive component comprises a porosity of at most 5 vol % and a content of the abrasive particles in a range between 2 vol % to 50 vol % for a total volume of the abrasive component.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 22, 2018
From: XIAO, JI; LUO, AIYUN; GOSAMO, IGNAZIO; SUSEK, VIVIAN
To: SAINT-GOBAIN ABRASIVES, INC.; SAINT-GOBAIN ABRASIFS
Reel/Frame 045664/0473 →
Priority Claims (1)
CN 2016 1 1222046 · Dec 26, 2016 · national
Continuity (2)
Provisional Application 62450910 · Jan 26, 2017
Related Publication 20180178348A1 · Jun 28, 2018