US2021062314A1PendingUtilityA1
Austenitic heat resistant alloy
Est. expiryDec 28, 2037(~11.4 yrs left)· nominal 20-yr term from priority
C22C 38/50C22C 38/44C22C 38/42C22C 38/06C22C 38/04C22C 38/02C22C 38/005C22C 38/002C22C 38/001C22C 38/54C23C 8/18C22C 38/48
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Claims
Abstract
There is provided an austenitic heat resistant alloy having a chemical composition that contains, in mass percent: C: 0.03 to 0.25%, Si: 0.01 to 2.0%, Mn: 0.10 to 0.50%, P: 0.030% or less, S: 0.010% or less, Cr: 13.0 to 30.0%, Ni: 25.0 to 45.0%, Al: 2.5 to 4.5%, Nb: 0.01 to 2.00%, N: 0.05% or less, Ti: 0 to 0.20%, W: 0 to 6.0%, Mo: 0 to 4.0%, Zr: 0 to 0.10%, B: 0 to 0.0100%, Cu: 0 to 5.0%, REM: 0 to 0.10%, Ca: 0 to 0.050%, Mg: 0 to 0.050%, and the balance: Fe and impurities.
Claims
exact text as granted — not AI-modified1 . An austenitic heat resistant alloy having a chemical composition consisting of, in mass percent:
C: 0.03 to 0.25%; Si: 0.01 to 2.0%; Mn: 0.10 to 0.50%; P: 0.030% or less; S: 0.010% or less; Cr: 13.0 to 30.0%; Ni: 25.0 to 45.0%; Al: 2.5 to 4.5%; Nb: 0.05 to 2.00%; N: 0.05% or less; Ti: 0 to 0.20%; W: 0 to 6.0%; Mo: 0 to 4.0%; Zr: 0 to 0.10%; B: 0 to 0.0100%; Cu: 0 to 5.0%; REM: 0 to 0.10%; Ca: 0 to 0.050%; Mg: 0 to 0.050%; and the balance: Fe and impurities.
2 . The austenitic heat resistant alloy according to claim 1 , wherein the chemical composition contains, in mass percent, B: 0.0010 to 0.0100%.
3 . The austenitic heat resistant alloy according to claim 1 or claim 2 , wherein in a case where the alloy is heated in an atmosphere containing steam at 900° C. for 20 hours and subsequently heated in an H 2 —CH 4 —CO2 atmosphere at 1100° C. for 96 hours, a continuous alumina layer having a thickness ranging from 0.5 to 15 μm is formed on a surface of the alloy.
4 . The austenitic heat resistant alloy according to claim 3 , wherein in the case where the alloy is heated in the atmosphere containing steam at 900° C. for 20 hours and subsequently heated in the H 2 —CH 4 —CO 2 atmosphere at 1100° C. for 96 hours, a layer having a Cr—Mn-based spinel structure formed on the alumina layer has a thickness of 5 μm or less.
5 . The austenitic heat resistant alloy according to claim 2 , wherein in a case where the alloy is heated in an atmosphere containing steam at 900° C. for 20 hours and subsequently heated in an H 2 —CH 4 —CO 2 atmosphere at 1100° C. for 96 hours, a continuous alumina layer having a thickness ranging from 0.5 to 15 μm is formed on a surface of the alloy.
6 . The austenitic heat resistant alloy according to claim 5 , wherein in the case where the alloy is heated in the atmosphere containing steam at 900° C. for 20 hours and subsequently heated in the H 2 —CH 4 —CO 2 atmosphere at 1100° C. for 96 hours, a layer having a Cr—Mn-based spinel structure formed on the alumina layer has a thickness of 5 μm or less.
7 . An austenitic heat resistant alloy having a chemical composition comprising, in mass percent:
C: 0.03 to 0.25%; Si: 0.01 to 2.0%; Mn: 0.10 to 0.50%; P: 0.030% or less; S: 0.010% or less; Cr: 13.0 to 30.0%; Ni: 25.0 to 45.0%; Al: 2.5 to 4.5%; Nb: 0.05 to 2.00%; N: 0.05% or less; Ti: 0 to 0.20%; W: 0 to 6.0%; Mo: 0 to 4.0%; Zr: 0 to 0.10%; B: 0 to 0.0100%; Cu: 0 to 5.0%; REM: 0 to 0.10%; Ca: 0 to 0.050%; Mg: 0 to 0.050%; and the balance: Fe and impurities.Join the waitlist — get patent alerts
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