Synthesis and processing of ultra high hardness boron carbide

Patent metadata

Field	Value
Publication number	US-9604885-B2
Application number	US-201414763540-A
Country	US
Kind code	B2
Filing date	Jan 27, 2014
Priority date	Jan 25, 2013
Publication date	Mar 28, 2017
Grant date	Mar 28, 2017

Abstract

A super-hard material is a late transition metal doped B 4 C ceramic. The lightweight ceramics can display Vickers Hardness in excess of 45 GPa. Transition metals, such as Ni, Co, Rh, and Pd can be doped into the boron carbide at levels up to about 2.5%. A spark plasma sintering (SPS) of an evacuated powder of B 4 C and the transition metal at temperatures up to 2000° C., and pressures of up to about 100 GPa forms a super-hard material as a body. The late transition metal doped B 4 C ceramic can be used for armor, grinding materials, thermoelectric materials, and catalysts.

First claim

We claim:

1. A super-hard material, comprising a single phase late transition metal doped boron carbide, wherein the Vickers Hardness is greater than 35 GPa, wherein the late transition metal is Ni, Co, Rh, Pd, or other Group 9 or Group 10 transition metal.

2. The super-hard material of claim 1 , wherein the boron carbide is B 4 C.

3. The super-hard material of claim 1 , wherein the late transition metal is 0.5 to 2 atom %.

4. The super-hard material of claim 1 , wherein the late transition metal is Ni at 1 atom %.

5. The super-hard material of claim 1 , wherein the Vickers Hardness is greater than 45 GPa.

6. A method for preparing a super-hard material comprises:
preparing a mixture of a late transition metal and B 4 C powder, wherein the late transition metal is Ni, Co, Rh, Pd or other Group 9 or Group 10 transition metal;
loading a die assembly with the powder;
placing said die assembly in a sintering chamber of a spark plasma sintering (SPS) apparatus;
evacuating the chamber; and
applying a pulsed current, pressure, and heat.

7. The method of claim 6 , wherein the late transition metal is 0.5 to 2 atom % of the mixture.

8. The method of claim 6 , wherein the sintering chamber is evacuated to 40 Pa or less.

9. The method of claim 6 , wherein heating is to 1,000 to 2,000° C.

10. The method of claim 6 , wherein the maximum pressure is 100 GPa.

11. An armor component, comprising a single phase late transition metal doped boron carbide with a Vickers Hardness in excess of 35 GPa, wherein the late transition metal is Ni, Co, Rh, Pd, or other Groin 9 or Group 10 transition metal.

12. A cutting medium, comprising a single phase late transition metal doped boron carbide with a Vickers Hardness in excess of 35 GPa, wherein the late transition metal is Ni, Co, Rh, Pd or other Group 9 or Group 10 transition metal.

Assignees

• Univ Florida
• Univ Central Florida Res Found Inc

Inventors

• Subhash Ghatu
• Blair Richard

Classifications

• F41H5/0492

  Layered armour containing hard elements, e.g. plates, spheres, rods, separated from each other, the elements being connected to a further flexible layer or being embedded in a plastics or an elastomer matrix · CPC title

• C04B2235/77

  Density · CPC title

• C04B2235/3821

  Boron carbides · CPC title

• C04B35/645

  Pressure sintering · CPC title

• C04B2235/5445

  submicron sized, i.e. from 0,1 to 1 micron · CPC title