US2004033158A1PendingUtilityA1
Precipitation hardened Co-Ni based heat-resistant alloy and production method therefor
Priority: Jul 5, 2002Filed: Jul 3, 2003Published: Feb 19, 2004
Est. expiryJul 5, 2022(expired)· nominal 20-yr term from priority
C22F 1/10C22C 19/056C22C 19/07C22C 30/00C22C 19/055
45
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Claims
Abstract
A precipitation hardened Co—Ni based heat-resistant alloy is composed of, all by weight, not more than 0.05% of C; not more than 0.5% of Si; not more than 1.0% of Mn; 25 to 45% of Ni; 13 to 22% of Cr; 10 to 18% of Mo or 10 to 18% of Mo+½W; 0.1 to 5.0% of Nb; 0.1 to 5.0% of Fe; and further at least one kind of 0.007 to 0.10% of REM; 0.001 to 0.010% of B; 0.0007 to 0.010% of Mg and 0.001 to 0.20% of Zr; the balance of substantially Co and inevitable impurities, and Co 3 Mo or Co 7 Mo 6 is precipitated in boundaries between a fine twin structure and a parent phase.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1 . A precipitation hardened Co—Ni based heat-resistant alloy comprising by weight:
not more than 0.05% of C; not more than 0.5% of Si; not more than 1.0% of Mn; 25 to 45% of Ni; 13 to 22% of Cr; 10 to 18% of Mo or 10 to 18% of Mo+½W; 0.1 to 5.0% of Nb; 0.1 to 5.0% of Fe;
at least one kind of 0.007 to 0.10% of REM; 0.001 to 0.010% of B; 0.0007 to 0.010% of Mg and 0.001 to 0.20% of Zr;
the balance of Co and inevitable impurities;
a fine twin structure;
a parent phase; and
Co 3 Mo or Co 7 Mo 6 precipitated at boundaries of the fine twin structure and the parent phase.
2 . A precipitation hardened Co—Ni based heat-resistant alloy comprising by weight:
not more than 0.05% of C; not more than 0.5% of Si; not more than 1.0% of Mn; 25 to 45% of Ni; 13 to 22% of Cr; 10 to 18% of Mo or 10 to 18% of Mo+½W; 0.1 to 5.0% of Nb; 0.1 to 5.0% of Fe; 0.1 to 3.0% of Ti;
at least one kind of 0.007 to 0.10% of REM; 0.001 to 0.010% of B; 0.0007 to 0.010% of Mg and 0.001 to 0.20% of Zr;
the balance of Co and inevitable impurities;
a fine twin structure;
a parent phase; and
Co 3 Mo or Co 7 Mo 6 precipitated at boundaries of the fine twin structure and the parent phase.
3 . A production method for precipitation hardened Co—Ni based heat-resistant alloy, the method comprising the steps of:
preparing an alloy comprising by weight:
not more than 0.05% of C; not more than 0.5% of Si; not more than 1.0% of Mn; 25 to 45% of Ni; 13 to 22% of Cr; 10 to 18% of Mo or 10 to 18% of Mo+½W; 0.1 to 5.0% of Nb; 0.1 to 5.0% of Fe;
at least one kind of 0.007 to 0.10% of REM; 0.001 to 0.010% of B; 0.0007 to 0.010% of Mg and 0.001 to 0.20% of Zr; and
the balance of Co and inevitable impurities;
subjecting the alloy to a solid solution heat treatment; and
subjecting the alloy to an aging heat treatment at 600 to 800° C. for 0.5 to 16 hours in a condition of applying stress, thereby forming a fine twin structure in a parent phase, and precipitating Co 3 Mo or Co 7 Mo 6 at a boundary of the fine twin structure and the parent phase.
4 . A production method for precipitation hardened Co—Ni based heat-resistant alloy, the method comprising the steps of:
preparing an alloy comprising by weight:
not more than 0.05% of C; not more than 0.5% of Si; not more than 1.0% of Mn; 25 to 45% of Ni; 13 to 22% of Cr; 10 to 18% of Mo or 10 to 18% of Mo+½W; 0.1 to 5.0% of Nb; 0.1 to 5.0% of Fe; 0.1 to 3.0% of Ti;
at least one kind of 0.007 to 0.10% of REM; 0.001 to 0.010% of B; 0.0007 to 0.010% of Mg and 0.001 to 0.20% of Zr; and
the balance of Co and inevitable impurities;
subjecting the alloy to a solid solution heat treatment; and
subjecting the alloy to an aging heat treatment at 600 to 800° C. for 0.5 to 16 hours in a condition of applying stress, thereby forming a fine twin structure in a parent phase, and precipitating Co 3 Mo or Co 7 Mo 6 at a boundary of the fine twin structure and the parent phase.
5 . A production method for precipitation hardened Co—Ni based heat-resistant alloy, the method comprising the steps of:
preparing an alloy comprising by weight:
not more than 0.05% of C; not more than 0.5% of Si; not more than 1.0% of Mn; 25 to 45% of Ni; 13 to 22% of Cr; 10 to 18% of Mo or 10 to 18% of Mo+½W; 0.1 to 5.0% of Nb; 0.1 to 5.0% of Fe;
at least one kind of 0.007 to 0.10% of REM; 0.001 to 0.010% of B; 0.0007 to 0.010% of Mg and 0.001 to 0.20% of Zr; and
the balance of Co and inevitable impurities;
subjecting the alloy to a solid solution heat treatment;
subjecting the alloy to a cold working or a warm working having a reduction ratio of not less than 40%; and
subjecting the alloy to an aging heat treatment at 600 to 800° C. for 0.5 to 16 hours in a condition of applying stress, thereby forming a fine twin structure in a parent phase, and precipitating Co 3 Mo or Co 7 Mo 6 at a boundary of the fine twin structure and the parent phase.
6 . A production method for precipitation hardened Co—Ni based heat-resistant alloy, the method comprising the steps of:
preparing an alloy comprising by weight:
not more than 0.05% of C; not more than 0.5% of Si; not more than 1.0% of Mn; 25 to 45% of Ni; 13 to 22% of Cr; 10 to 18% of Mo or 10 to 18% of Mo+½W; 0.1 to 5.0% of Nb; 0.1 to 5.0% of Fe; 0.1 to 3.0% of Ti.
at least one kind of 0.007 to 0.10% of REM; 0.001 to 0.010% of B; 0.0007 to 0.010% of Mg and 0.001 to 0.20% of Zr; and
the balance of Co and inevitable impurities;
subjecting the alloy to a solid solution heat treatment;
subjecting the alloy to a cold working or a warm working having a reduction ratio of not less than 40%; and
subjecting the alloy to an aging heat treatment at 600 to 800° C. for 0.5 to 16 hours in a condition of applying stress, thereby forming a fine twin structure in a parent phase, and precipitating Co 3 Mo or Co 7 Mo 6 at a boundary of the fine twin structure and the parent phase.
7 . A production method for precipitation hardened Co—Ni based heat-resistant alloy, the method comprising the steps of:
preparing an alloy comprising by weight:
not more than 0.05% of C; not more than 0.5% of Si; not more than 1.0% of Mn; 25 to 45% of Ni; 13 to 22% of Cr; 10 to 18% of Mo or 10 to 18% of Mo+½W; 0.1 to 5.0% of Nb; 0.1 to 5.0% of Fe;
at least one kind of 0.007 to 0.10% of REM; 0.001 to 0.010% of B; 0.0007 to 0.010% of Mg and 0.001 to 0.20% of Zr; and
the balance of Co and inevitable impurities;
subjecting the alloy to a solid solution heat treatment;
subjecting the alloy to a cold working or a warm working having a reduction ratio of not less than 40%; and
subjecting the alloy to an aging heat treatment at 800° C. to 950° C. for 0.5 to 16 hours, thereby forming a fine twin structure in a parent phase, and precipitating Co 3 Mo or Co 7 Mo 6 at a boundary of the fine twin structure and the parent phase.
8 . A production method for precipitation hardened Co—Ni based heat-resistant alloy, the method comprising the steps of:
preparing an alloy comprising: all by weight, not more than 0.05% of C; not more than 0.5% of Si; not more than 1.0% of Mn; 25 to 45% of Ni; 13 to 22% of Cr; 10 to 18% of Mo or 10 to 18% of Mo+½W; 0.1 to 5.0% of Nb; 0.1 to 5.0% of Fe; 0.1 to 3.0% of Ti;
at least one kind of 0.007 to 0.10% of REM; 0.001 to 0.010% of B; 0.0007 to 0.010% of Mg and 0.001 to 0.20% of Zr; and
the balance of Co and inevitable impurities;
subjecting the alloy to a solid solution heat treatment;
subjecting the alloy to a cold working or a warm working having a reduction ratio of not less than 40%; and
subjecting the alloy to an aging heat treatment at 800° C. to 950° C. for 0.5 to 16 hours, thereby forming a fine twin structure in a parent phase, and precipitating Co 3 Mo or Co 7 Mo 6 at a boundary of the fine twin structure and the parent phase.Join the waitlist — get patent alerts
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