2012
DOI: 10.1016/j.jallcom.2011.09.094
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Microstructural evolution in damaged IN738LC alloy during various steps of rejuvenation heat treatments

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Cited by 38 publications
(12 citation statements)
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“…There are other types of carbides such as M 6 C, where M denotes Si, Ni and Cr, and also M 23 C 6 where M denotes mainly Cr and/or Mo. [6][7][8][9] Nevertheless, the high cost of nickel based superalloys makes them unviable for massive applications in some situations. In order to overcome this obstacle and make the use of Ni-based alloys attractive to equipment manufacturers, providing high service performance using this particular class of material, overlays with Ni-based alloys on C-Mn low alloy and stainless steels have become an option in recent years.…”
Section: Introductionmentioning
confidence: 99%
“…There are other types of carbides such as M 6 C, where M denotes Si, Ni and Cr, and also M 23 C 6 where M denotes mainly Cr and/or Mo. [6][7][8][9] Nevertheless, the high cost of nickel based superalloys makes them unviable for massive applications in some situations. In order to overcome this obstacle and make the use of Ni-based alloys attractive to equipment manufacturers, providing high service performance using this particular class of material, overlays with Ni-based alloys on C-Mn low alloy and stainless steels have become an option in recent years.…”
Section: Introductionmentioning
confidence: 99%
“…[1][2][3] In order to obtain much more excellent resistance to primary water stress corrosion cracking in the nuclear power industry, steam generator and pressurised water reactor systems, nickel base alloys with high chromium were developed. 4,5 However, unfortunately, as confirmed by industry experience and laboratory investigation, the high chromium nickel base alloys were susceptible to hot cracking during welding.…”
Section: Introductionmentioning
confidence: 99%
“…The solution heat treatments are designed to dissolve γ'/γ eutectic, γ' and carbide phases and allow the optimum reprecipitation of these phases upon cooling or after ageing. According to Table 2, four different heat treatment cycles including aging (A) [11], partial (B) [12], full (C) [4], and partial + full (D) [13] solution treatments followed by aging at 900° C for 10h were applied to the as-cast alloy. Metallographic sections were prepared using standard polishing procedures according to ASTM E3-01.…”
Section: Methodsmentioning
confidence: 99%