Method for producing composite materials consisting of continuous silicon carbide fibers and beryllium

Claim 3

A method according to claim 1, wherein said matrix is at least one member selected from beryllium and alloys of beryllium with calcium, tungsten, molybdenum, iron, cobalt, nickel, chromium, silver, copper, manganese, zirconium, niobium and yttrium.

Claim 4

A method according to claim 2, wherein the amount of the metal to be alloyed with beryllium is 0.1-30% by weight based on the weight of the alloy.

Claim 5

A method according to claim 1, wherein said spun fibers are produced from organosilicon high molecular weight compounds having silicon and carbon as the main skeleton components, which are produced from at least one of organosilicon low molecular weight compounds of the following groups (1)-(10), (1) Compounds having only Si--C bond, (2) Compounds having Si--H bond in addition to Si--C bond, (3) Compounds having Si--Hal bond, (4) Compounds having Si--N bond, (5) Compounds having Si--OR (R is alkyl or aryl group) bond, (6) Compounds having Si--OH bond, (7) Compounds having Si--Si bond, (8) Compounds having Si--O--Si bond, (9) Esters of organosilicon compounds and (10) Peroxides of organosilicon compounds, by polycondensation reaction using at least one process or irradiation, heating and addition of a catalyst for the polycondensation.

Claim 6

A method according to claim 1, wherein an assembly composed of the matrix and the continuous silicon carbide fibers are sintered or hot pressed under vacuum or an inert atmosphere to bond tightly the matrix to the fibers.

Claim 7

A method according to claim 1, foils or thin sheets of the matrix material and the continuous silicon carbide fibers are regularly superposed and hot pressed or hot rolled under vacuum or an inert atmosphere to diffuse and bond the matrix material and the fibers tightly.

Claim 8

A method according to claim 1, wherein the matrix material is coated or sprayed by plasma on each of the continuous silicon carbide fibers, and the resulting fibers are gathered and hot pressed under vacuum or an inert atmosphere.

Claim 9

A beryllium composite material reinforced with continuous silicon carbide fibers, which consists mainly of the following three components, (a) continuous silicon carbide fibers consisting mainly of β-type silicon carbide fine particles of less than 1,000 A in diameter obtained by baking spun fibers consisting mainly of organosilicon high molecular weight compound, (b) beryllium matrix selected from the group consisting of beryllium, beryllium alloys and composites consisting mainly of beryllium, and (c) a very small amount of carbide which is formed by reacting free carbon contained in the surface of the continuous silicon carbide fibers with the matrix beryllium or beryllium alloys.

Claim 10

A beryllium composite material reinforced with continuous silicon carbide fibers, which consists mainly of the following three components, (a) continuous silicon carbide fibers consisting mainly of β-type silicon carbide fine particles of less than 1,000 A in diameter obtained by baking spun fibers consisting mainly of organosilicon high molecular weight compound, (b) beryllium matrix selected from the group consisting of beryllium, beryllium alloys and composites consisting mainly of beryllium, and (c) a very small amount of carbide which is formed by reacting free carbon contained in the surface of the continuous silicon carbide fibers with the matrix beryllium or beryllium alloys.

Claim 11

A beryllium composite material according to claim 8, wherein said beryllium composite material has a high oxidation resistance and has a hardness of 6-9 mohs, a tensile strength of 110-310 kg/mm 2 at temperature under 900° C., and a thermal conductivity of (0.22-0.10) cal/cm.sec°

Claim 12

A beryllium composite material according to claim 8, which is used as a material for aerospace instrument and a material for nuclear industry.