CPC B22F 5/009 (2013.01) [B22F 1/142 (2022.01); B22F 9/082 (2013.01); C21D 1/18 (2013.01); C21D 6/004 (2013.01); C21D 6/02 (2013.01); C22C 19/055 (2013.01); C22C 19/056 (2013.01); C22C 30/00 (2013.01); C22C 30/02 (2013.01); C22C 38/004 (2013.01); C22C 38/02 (2013.01); C22C 38/04 (2013.01); C22C 38/06 (2013.01); C22C 38/42 (2013.01); C22C 38/44 (2013.01); C22C 38/48 (2013.01); C22C 38/50 (2013.01); C22C 38/52 (2013.01); F01D 5/28 (2013.01); B22F 3/04 (2013.01); B22F 3/10 (2013.01); B22F 3/15 (2013.01); B22F 3/225 (2013.01); B22F 2301/35 (2013.01); B22F 2998/10 (2013.01); B22F 2999/00 (2013.01); F04D 29/02 (2013.01); F05D 2300/17 (2013.01)] | 9 Claims |
1. A process for making a component of a turbomachine, the process comprising the steps of:
a) melting an alloy chemical composition consisting of:
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based on the composition weight, the remaining being Fe and impurities, the impurities comprising S 0.0-0.01 wt % and P 0.0-0.025 wt %, through vacuum induction melting (VIM), or arc electric furnace,
b) refining by Argon Oxygen Decarburization (A.O.D.), Vacuum Induction Degassing and Pouring (V.I.D.P), or Vacuum Oxygen Decarburization (V.O.D.),
c) re-melting through electro-slag re-melting (E.S.R.), or vacuum arc re-melting (VAR),
d) heat-treating the alloy resulting from step c) to induce solubilization through at least one heat cycle, at a temperature of 1020-1150° C., and followed by fast cooling in liquid or gas media, and
e) ageing by heating to a temperature of 600-700° C. for 2-20 h, and
f) immediately cooling the alloy resulting from step e) at room temperature.
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