| CPC C22C 38/60 (2013.01) [C21D 1/02 (2013.01); C21D 1/26 (2013.01); C21D 6/004 (2013.01); C21D 8/0205 (2013.01); C21D 1/60 (2013.01); C21D 8/0242 (2013.01); C21D 8/0247 (2013.01); C21D 9/46 (2013.01); C22C 38/002 (2013.01); C22C 38/005 (2013.01); C22C 38/02 (2013.01); C22C 38/04 (2013.01); C22C 38/42 (2013.01); C22C 38/44 (2013.01); C22C 38/46 (2013.01); C22C 38/48 (2013.01); C22C 38/52 (2013.01); C22C 38/54 (2013.01)] | 5 Claims |

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1. An alloy material having a chemical composition consisting of, in mass %,
C: 0.010 to 0.10%,
Si: more than 0.10% to 0.50% or less,
Mn: 0.05 to 0.50%,
P: 0.015% or less,
S: 0.0015% or less,
Cr: 0.005 to 0.50%,
Ni: 34.5 to 37.0%,
Cu: 0.005 to 1.0%,
Co: 0.005 to 0.50%,
Mo: 0.001 to 0.50%,
Al: 0.0001 to 0.050%,
Nb: 0.001 to 1.0%,
N: 0.010% or less,
O: 0.0060% or less,
Ti: 0.0200% or less,
Zr: 0.0200% or less,
Hf: 0.0200% or less,
V: 0.500% or less,
W: 1.000% or less,
Sn: 0.050% or less,
Zn: 0.0020% or less,
Pb: 0.0010% or less,
Ta: 0 to 1.0%,
B: 0 to 0.010%,
Ca: 0 to 0.0050%,
Mg: 0 to 0.0030%,
REM: 0 to 0.050%, and
the balance: Fe and unavoidable impurities,
and satisfying Formula (1), Formula (2), Formula (3) and Formula (4) below,
wherein:
a yield stress is 240 MPa or more, and
a plate thickness is 3.0 mm or more;
T0≤T1-2 (1)
C—Nb/7.7-Ta/15≤0.045 (2)
Nb-7.7C≤0.30 (3)
Ta-15C≤0.30 (4)
where, each symbol of an element in the above formulas represents a content, in mass %, of a corresponding element, T0 represents a Curie temperature, in ° C., of the alloy material, and T1 represents a Curie temperature, in ° C., of the alloy material after the alloy material is held at 900° C. for one minute and thereafter is cooled under conditions such that an average cooling rate in a temperature range from 600 to 300° C. is 0.2° C./s.
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