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US3993475A Expired / Lapsed US ⏱️ 0.0 years remaining

Heat resisting alloys

Assignee: Duraloy Co
•
Filing: 1975-04-18
•
Granted: 1976-11-23
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Expires: 1995-04-18
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Abstract

Abstract A new alloy is provided having high creep strength at elevated temperatures in the range 1100 DEG to 1200 DEG C. and which is unusually resistant to corrosion and thermal shock and has unusual stress rupture characteristics at the elevated temperatures here involved consisting essentially of, by weight, about 0.3% to 0.9% carbon, 20% to 30% chromium, 26% to 40% nickel, 0.8% to 4.0% manganese, 0.9% to 3.5% silicon, 0.3% to 5.0% tungsten, 3.5% to 8.5% cobalt and the balance iron with residual impurities in ordinary amounts.

Inventors

  • 👤 Kohsaburo Harada
  • 👤 Yousuke Matsumoto
  • 👤 Rokurou Kiyoshima

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-06 00:38
CPC Classifications
C; C22; C22C; C22C30/00

Claims Analysis

Total Claims: 9
Claim 1
Independent Claim 91 words
An alloy characterized by high creep strength at elevated temperatures in the range 1,100° C. to 1,200° C., by resistance to corrosion, particularly in the form of oxidation, by resistance to thermal shock and by unusual stress rupture characteristics at elevated temperatures consisting of, by weight, about 0.3% to 0.9% carbon, about 20% to 30% chromium, about 26% to 40% nickel, about 0.8% to 4.0% manganese, about 0.9% to 3.5% silicon, about 0.3% to 5.0% tungsten, about 3.5% to 8.5% cobalt and the balance iron with residual impurities in ordinary amounts.
Claim 2
Dependent Claim 91 words
An alloy characterized by high creep strength at elevated temperatures in the range 1,100° C. to 1,200° C., by resistance to corrosion, particularly in the form of oxidation, by resistance to thermal shock and by unusual stress rupture characteristics at elevated temperatures consisting of, by weight, about 0.3% to 0.9% carbon, about 20% to 30% chromium, about 26% to 40% nickel, about 0.8% to 4.0% manganese, about 0.9% to 3.5% silicon, about 0.3% to 5.0% tungsten, about 3.5% to 8.5% cobalt and the balance iron with residual impurities in ordinary amounts.
Claim 3
Dependent Claim 14 words
An alloy as claimed in claim 1 having 0.3% to 2.5% by weight niobium.
Claim 4
Dependent Claim 107 words
An alloy article for use at elevated temperatures in the range 1,100° to 1,200° C. made from an alloy characterized by high creep strength at elevated temperatures in the range 1,100° to 1,200° C., by resistance to corrosion, particularly in the form of oxidation, by resistance to thermal shock and by unusual stress rupture characteristics at elevated temperatures consisting of, by weight, about 0.3% to 0.9% carbon, about 20% to 30% chromium, about 26% to 40% nickel, about 0.8% to 4.0% manganese, about 0.9% to 3.5% silicon, about 0.3% to 5.0% tungsten, about 3.5% to 8.5% cobalt and the balance iron with residual impurities in ordinary amounts.
Claim 5
Dependent Claim 107 words
An alloy article for use at elevated temperatures in the range 1,100° to 1,200° C. made from an alloy characterized by high creep strength at elevated temperatures in the range 1,100° to 1,200° C., by resistance to corrosion, particularly in the form of oxidation, by resistance to thermal shock and by unusual stress rupture characteristics at elevated temperatures consisting of, by weight, about 0.3% to 0.9% carbon, about 20% to 30% chromium, about 26% to 40% nickel, about 0.8% to 4.0% manganese, about 0.9% to 3.5% silicon, about 0.3% to 5.0% tungsten, about 3.5% to 8.5% cobalt and the balance iron with residual impurities in ordinary amounts.
Claim 6
Dependent Claim 15 words
An alloy article as claimed in claim 3 containing 0.3% to 2.5% by weight niobium.
Claim 7
Dependent Claim 107 words
A structural member for use at elevated temperature in the range 1,100° to 1,200° C. made from an alloy characterized by high creep strength at elevated temperatures in the range 1,100° to 1,200° C., by resistance to corrosion, particularly in the form of oxidation, by resistance to thermal shock and by unusual stress rupture characteristics at elevated temperatures consisting of, by weight, about 0.3% to 0.9% carbon, about 20% to 30% chromium, about 26% to 40% nickel, about 0.8% to 4.0% manganese, about 0.9% to 3.5% silicon, about 0.3% to 5.0% tungsten, about 3.5% to 8.5% cobalt and the balance iron with residual impurities in ordinary amounts.
Claim 8
Dependent Claim 107 words
A structural member for use at elevated temperature in the range 1,100° to 1,200° C. made from an alloy characterized by high creep strength at elevated temperatures in the range 1,100° to 1,200° C., by resistance to corrosion, particularly in the form of oxidation, by resistance to thermal shock and by unusual stress rupture characteristics at elevated temperatures consisting of, by weight, about 0.3% to 0.9% carbon, about 20% to 30% chromium, about 26% to 40% nickel, about 0.8% to 4.0% manganese, about 0.9% to 3.5% silicon, about 0.3% to 5.0% tungsten, about 3.5% to 8.5% cobalt and the balance iron with residual impurities in ordinary amounts.
Claim 9
Dependent Claim 15 words
A structural member as claimed in claim 5 containing 0.3% to 2.5% by weight niobium.

References Cited (Backward Citations)

US2504453A Cited
US2481976A Cited
US2860968A Cited
US3366473A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1979-11-23 1980-05-24 1980-11-23 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1983-11-23 1984-05-24 1984-11-23 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1987-11-23 1988-05-24 1988-11-23 $7700.00 Window Closed / Lapsed

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