US4487644A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Binderless weld-bonding of preshaped sic-base parts into solid bodies
Assignee: Forschungszentrum Jülich
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Filing: 1982-09-24
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Granted: 1984-12-11
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Expires: 2002-09-24
Abstract
Abstract Component bodies of silicon carbide base material, at least in their surface layers, are welded together without the provision of a binder at finely polished joining surfaces by virtue of the fact that at least one of the joint surfaces is of a silicon carbide material containing an excess of silicon (SiSiC). The component bodies are kept closely fitted together especially by an additional pressing force of at least 0.1 kg/cm 2 during a heating stage at atmospheric or lower pressure at a temperature in the range from 1500° C. to 1800° C. for 15 to 100 minutes in an inert atmosphere, the excess of silicon at the boundary making it possible for silicon carbide crystal growth to take place across the boundary.
Inventors
- 👤 Ashok K. Gupta
- 👤 Ernoe Gyarmati
- 👤 Hermann Kreutz
- 👤 Rudolf Muenzer
- 👤 Aristides Naoumidis
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-27 16:20
CPC Classifications
C; C04; C04B; C04B35/00; C04B35/515; C04B35/56; C04B35/565; C04B35/573; C04B37/00; C04B37/001; C04B2235/00; C04B2235/65; C04B2235/656; C04B2235/6567; C04B2235/658; C04B2235/6581; C04B2237/00; C04B2237/30; C04B2237/32; C04B2237/36; C04B2237/365; C04B2237/50; C04B2237/52; C04B2237/525; C04B2237/56; C04B2237/568
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 .
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1987-12-11 | 1988-06-11 | 1988-12-11 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1991-12-11 | 1992-06-11 | 1992-12-11 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1995-12-11 | 1996-06-11 | 1996-12-11 | $7700.00 | Window Closed / Lapsed |