Boron carbide based sintered compact and method for preparation thereof
Abstract
A boron carbide based sintered body having a four-point flexural strength of at least 400 MPa and a fracture toughness of at least 2.8 MPa·m 1/2 , which has the following two preferred embodiments. (1) A boron carbide-titanium diboride sintered body obtained by sintering a mixed powder of a B 4 C powder, a TiO 2 powder and a C powder while reacting them under a pressurized condition and comprising from 95 to 70 mol % of boron carbide and from 5 to 30 mol % of titanium diboride, wherein the boron carbide has a maximum particle diameter of at most 5 μm. (2) A boron carbide-chromium diboride sintered body containing from 10 to 25 mol % of CrB 2 in B 4 C, wherein the sintered body has a relative density of at least 90%, boron carbide particles in the sintered body have a maximum particle diameter of at most 100 μm, and the abundance ratio (area ratio) of boron carbide particles of from 10 to 100 μm to boron carbide particles having a particle diameter of at most 5 μm, is from 0.02 to 0.6.
Claims
exact text as granted — not AI-modified1 . A boron carbide based sintered body characterized by having a four point flexural strength of at least 400 MPa as measured in accordance with JIS R1601 and a fracture toughness of at least 2.8 MPa·m 1/2 as measured in accordance with JIS R1607-SEPB method.
2 . The boron carbide based sintered body according to claim 1 , which is a boron carbide-titanium diboride sintered body obtained by sintering a mixed powder of boron carbide (B 4 C) powder, titanium dioxide (TiO 2 ) powder and carbon (C) powder while reacting them under a pressurized condition and which comprises from 95 to 70 mol % of boron carbide and from 5 to 30 mol % of titanium diboride, wherein the boron carbide has a maximum particle diameter of at most 5 μm.
3 . The boron carbide based sintered body according to claim 1 or 2 , wherein the four point flexural strength is at least 700 MPa.
4 . The boron carbide based sintered body according to claim 1 , 2 or 3 , wherein the four point flexural strength is at least 800 MPa, and the fracture toughness is at least 3.0 MPa·m 1/2 .
5 . A boron carbide based sintered body which is a boron carbide-chromium diboride sintered body containing from 10 to 25 mol % of chromium diboride (CrB 2 ) in boron carbide (B 4 C), characterized in that the sintered body has a relative density of at least 90%, boron carbide particles in the sintered body have a maximum particle diameter of at most 100 μm, and the abundance ratio (area ratio) of boron carbide particles of from 10 to 100 μm to boron carbide particles having a particle diameter of at most 5 μm, is from 0.02 to 0.6.
6 . The boron carbide based sintered body according to claim 5 , which has an electric conductivity of at least 5×10 2 S/m.
7 . The boron carbide based sintered body according to claim 6 , which has a four point flexural strength of at least 400 MPa and a fracture toughness of at least 3.0 MPa·m 1/2 .
8 . A process for producing a boron carbide based sintered body, characterized by mixing a titanium dioxide powder having an average particle diameter of less than 1 μm and a carbon powder having an average particle diameter of less than 1 μm to a boron carbide powder having a maximum particle diameter of at most 5 μm, an average particle diameter of at most 1 μm and a specific surface area of at least 10 m 2 /g, and sintering the mixture within a temperature range of from 1900 to 2100° C. while reacting them under a pressurized condition.
9 . The process for producing a boron carbide based sintered body according to claim 8 , wherein the specific surface area of the boron carbide powder is at least 16 m 2 /g, and the average particle diameter of each of the titanium dioxide powder and the carbon powder is less than 0.1 μm.
10 . A process for producing a boron carbide based sintered body, characterized by molding a raw material powder having from 10 to 25 mol % of a chromium diboride powder added and mixed to a boron carbide powder having an average particle diameter (D 50 ) of at most 2 μm and a specific surface area of at least 10 m 2 /g, followed by heating from 1950 to 2100° C. in a non-oxidizing atmosphere under a non-pressurized condition.
11 . A shock absorber made of the boron carbide based sintered body as defined in any one of claims 1 to 7 .
12 . The shock absorber according to claim 11 , wherein the shock absorber is for a high velocity missile.
13 . An abrasion resistant component made of the boron carbide based sintered body as defined in any one of claims 1 to 7 .Cited by (0)
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