Ferritic stainless steel for fuel cell and method for producing the same
US-2017321310-A1 · Nov 9, 2017 · US
US10501831B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10501831-B2 |
| Application number | US-201515517405-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 16, 2015 |
| Priority date | Oct 8, 2014 |
| Publication date | Dec 10, 2019 |
| Grant date | Dec 10, 2019 |
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The invention relates to a microstructure of an alloy for a tube for reformers, having an austenitic matrix structure, characterised in that: i) primary micrometric precipitates in the form of M 23 C 6 -type carbides, where M=Fe, Ni or Cr, and/or M(C,N)-type carbides, where M==Nb or Ti, are formed during the solidification of the alloy; ii) secondary nanometric precipitates in the form of M 23 C 6 -type carbides, where M=Fe, Ni or Cr and/or M(C,N)-type carbides, where M==Nb or Ti, are formed during the activation of the tube; and iii) between 0.1 and 0.3% of Ni 16 Si7Nb 6 -type intermetallic precipitates is formed during the use of the tube.
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The invention claimed is: 1. A process for the manufacture of an alloy of iron, nickel and chromium, for a tube of reformers, comprising from 22 to 30% by weight of Cr, from 20 to 45% by weight of Ni and from 0.3 to 0.6% by weight of C and exhibiting a microstructure with an austenitic matrix such that: i) micrometric primary precipitates in the form of carbides of M 23 C 6 type with M=Fe, Ni or Cr and/or of M(C,N) type with M=Nb or Ti are formed during the solidification of the alloy; ii) nanometric secondary precipitates in the form of carbides of M 23 C 6 type with M=Fe, Ni or Cr and of M(C,N) type with M=Nb or Ti are formed during the bringing into service of the tube; and iii) an amount of intermetallic precipitates of Ni 16 Si 7 Nb 6 type of between 0.1 and 0.3% is formed during the use of the tube, the process comprising a heat treatment of said alloy carried out in two stages: a) a first stage of heat treatment at temperatures between 700° C. and 800° C. with a stationary phase of 10 h to 100 h, and b) a second stage of heat treatment under operating conditions of the furnace of the reforming having as source a source of hydrocarbons and being subjected to a pressure varying between 1 and 4 MPa and a temperature between 900° C. and 1000° C. 2. The process of claim 1 , wherein the secondary precipitates form dislocation clusters. 3. The process of claim 1 , wherien the primary precipitates are micrometric. 4. The process of claim 1 , wherein the secondary precipitates are nanometric. 5. The process of claim 4 , wherein the secondary precipitates are between 5 nm and 50 nm. 6. The process of claim 1 , wherein the primary precipitates of M 23 C 6 type represents from 3 to 8% of the chemical composition of the alloy and the M(C,N) precipitates represents from 0.5 to 2.5% of the chemical composition of the alloy. 7. The process of claim 1 , wherein the secondary precipitates of M 23 C 6 type represents from 1 to 3% of the chemical composition of the alloy and the M(C,N) precipitates represents from 0.1 to 0.5% of the chemical composition of the alloy.
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