Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
195 words
Method of producing complex shaped bodies on a silicon carbide basis comprising the steps of: prefabricating integral component bodies with polished boundary surfaces for fitting together with each other and thereby forming boundary surfaces, said component bodies having their boundary surfaces composed of a material selected from the group of SiC and SiSiC, said composition being the same for at least a layer of the body adjoining the boundary surface, at least one component body of every pair of component bodies facing each other across a said boundary surface having a surface and at least a surface layer thereunder composed of SiSiC having excess silicon, with reference to the stoichiometric SiC composition, of at least 8% by weight, to a depth of about 10 μm, adjoining said boundary surface; fitting said components closely together without the interposition of a binder and without application of pressure in excess of 10 kg/cm 2 , and heating the fitted-together bodies in an inert atmosphere at a pressure between 10 -3 torr and 1 atmosphere at a temperature between 1500° C. and 1800° C. for not less than 15 minutes and not more than 100 minutes, followed by cooling.
Claim 2
Dependent Claim
195 words
Method of producing complex shaped bodies on a silicon carbide basis comprising the steps of: prefabricating integral component bodies with polished boundary surfaces for fitting together with each other and thereby forming boundary surfaces, said component bodies having their boundary surfaces composed of a material selected from the group of SiC and SiSiC, said composition being the same for at least a layer of the body adjoining the boundary surface, at least one component body of every pair of component bodies facing each other across a said boundary surface having a surface and at least a surface layer thereunder composed of SiSiC having excess silicon, with reference to the stoichiometric SiC composition, of at least 8% by weight, to a depth of about 10 μm, adjoining said boundary surface; fitting said components closely together without the interposition of a binder and without application of pressure in excess of 10 kg/cm 2 , and heating the fitted-together bodies in an inert atmosphere at a pressure between 10 -3 torr and 1 atmosphere at a temperature between 1500° C. and 1800° C. for not less than 15 minutes and not more than 100 minutes, followed by cooling.
Claim 3
Dependent Claim
25 words
Method as defined in claim 1, in which the pressure at which the heating step is performed is in the neighborhood of 10 -2 torr.
Claim 4
Dependent Claim
22 words
Method as defined in claim 1, in which the temperature of said heating step is maintained in the neighborhood of 1600° C.
Claim 5
Dependent Claim
52 words
Method as defined in claim 1, in which the step of fitting said component bodies together includes applying a pressure of at least 0.1 kg/cm 2 across each of the boundary surfaces where the component bodies are to be bonded together, and in which said pressure is maintained during the heat step.
Claim 6
Dependent Claim
32 words
Method as defined in claim 4, in which said pressure applied across said boundary surfaces and maintained during the heating step is in the range from 1 to 10 kg/cm 2 .
Claim 7
Dependent Claim
30 words
Method as defined in claim 5, in which said pressure applied across said boundary surfaces and maintained during the heating step is in the neighborhood of 5 kg/cm 2 .