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US4031178A Expired / Lapsed US ⏱️ 0.0 years remaining

Strength improvement in machined SiC bodies

Assignee: General Electric Co
•
Filing: 1976-04-09
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Granted: 1977-06-21
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Expires: 1996-04-09
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Abstract

Abstract A silicon carbide body with a density of at least 85% is machined to required specification and then fired at a temperature ranging from 1400° C to 2100° C in a firing atmosphere ranging in pressure from 10.sup. -3 torr to 25 torr to increase its fracture strength by at least 10%.

Inventors

  • 👤 Curtis A. Johnson
  • 👤 Svante Prochazka

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-27 08:39
CPC Classifications
C; C04; C04B; C04B35/00; C04B35/515; C04B35/56; C04B35/565; C04B35/575

Claims Analysis

Total Claims: 9
Claim 1
Independent Claim 144 words
A method for increasing the fracture strength of a machined polycrystalline silicon carbide body having a density of at least 85% of the theoretical density of silicon carbide and containing silicon carbide in an amount of at least 90% by weight of said body, machining said body inducing surface irregularities which significantly limit the fracture strength thereof, and firing said machined body in an atmosphere ranging in pressure from about 10 - 3 torr to 25 torr wherein the residual gases have no significant deteriorating effect on said silicon carbide body at a temperature ranging from about 1400° C to 2100° C to increase the fracture strength thereof at room temperature by at least about 10% compared to that of the as-machined body, said body being free of constituent which are not chemically inert nor undergoe significant melting or vaporization at said firing temperature.
Claim 2
Independent Claim 144 words
A method for increasing the fracture strength of a machined polycrystalline silicon carbide body having a density of at least 85% of the theoretical density of silicon carbide and containing silicon carbide in an amount of at least 90% by weight of said body, machining said body inducing surface irregularities which significantly limit the fracture strength thereof, and firing said machined body in an atmosphere ranging in pressure from about 10 - 3 torr to 25 torr wherein the residual gases have no significant deteriorating effect on said silicon carbide body at a temperature ranging from about 1400° C to 2100° C to increase the fracture strength thereof at room temperature by at least about 10% compared to that of the as-machined body, said body being free of constituent which are not chemically inert nor undergoe significant melting or vaporization at said firing temperature.
Claim 3
Dependent Claim 18 words
A method according to claim 1 wherein said pressure ranges from 10 - 2 torr to 1 torr.
Claim 4
Dependent Claim 17 words
A method according to claim 1 wherein said firing temperature ranges from 1700° C to 1900° C.
Claim 5
Dependent Claim 19 words
A method according to claim 1 wherein the density of said silicon carbide body ranges from 90 to 100%.
Claim 6
Dependent Claim 22 words
A method according to claim 1 wherein said residual gases are selected from the group consisting of carbon monoxide, argon and helium.
Claim 7
Dependent Claim 16 words
A method according to claim 1 wherein said polycrystalline silicon carbide body is a sintered body.
Claim 8
Dependent Claim 16 words
A method according to claim 1 wherein said polycrystalline silicon carbide body is a hot-pressed body.
Claim 9
Dependent Claim 17 words
A method according to claim 1 wherein said fracture strength is increased from about 10 to 30%.

References Cited (Backward Citations)

No citation records indexed.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1980-06-20 1980-12-20 1981-06-21 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1984-06-20 1984-12-20 1985-06-21 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1988-06-20 1988-12-20 1989-06-21 $7700.00 Window Closed / Lapsed

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