CPC B22F 1/00 (2013.01) [B22F 7/02 (2013.01); B22F 10/28 (2021.01); C22C 1/0433 (2013.01); C22C 19/055 (2013.01); C22C 19/056 (2013.01); B22F 2301/15 (2013.01); B22F 2303/01 (2013.01); B22F 2304/10 (2013.01); B22F 2999/00 (2013.01); B33Y 10/00 (2014.12); B33Y 70/00 (2014.12); B33Y 80/00 (2014.12)] | 2 Claims |
1. A composite member comprising:
a base material; and
an alloy layer laminated on a surface of the base material, wherein
the alloy layer which is a laminated model having a solidification structure, includes, by mass %,
Cr: 18 to 22%,
Mo: 18 to 28%,
Ta: 1.5 to 57%,
C: 1.0 to 2.5%
Nb: 0 to 42%,
Ti: 0 to 15%,
V: 0 to 27%,
Zr: 0 to 29%, and
a remainder consisting of Ni and unavoidable impurities, where a molar ratio of (Ta+0.7Nb+Ti+0.6V+Zr)/C=0.5 to 1.5 is satisfied, and wherein
the solidification structure is a dendrite crystal structure having a metal phase having a face-centered cubic structure and carbides including a carbide phase mainly containing any element of Ta, Nb, Ti, V, and Zr.
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