Influences of niobium and solution treatment temperature on pitting corrosion behaviour of stabilised austenitic stainless steels

2016 ◽  
Vol 108 ◽  
pp. 111-124 ◽  
Author(s):  
Guanshun Bai ◽  
Shanping Lu ◽  
Dianzhong Li ◽  
Yiyi Li

2007 ◽  
Vol 49 (4) ◽  
pp. 1718-1736 ◽  
Author(s):  
C. García ◽  
F. Martín ◽  
P. de Tiedra ◽  
L. García Cambronero


2007 ◽  
Vol 49 (2) ◽  
pp. 510-525 ◽  
Author(s):  
A. Pardo ◽  
M.C. Merino ◽  
M. Carboneras ◽  
A.E. Coy ◽  
R. Arrabal




2008 ◽  
Vol 50 (6) ◽  
pp. 1796-1806 ◽  
Author(s):  
A. Pardo ◽  
M.C. Merino ◽  
A.E. Coy ◽  
F. Viejo ◽  
R. Arrabal ◽  
...  




2010 ◽  
Vol 89-91 ◽  
pp. 377-382 ◽  
Author(s):  
S. Mineta ◽  
Shigenobu Namba ◽  
Takashi Yoneda ◽  
Kyosuke Ueda ◽  
Takayuki Narushima

Microstructural changes occurring in biomedical Co-Cr-Mo alloys with three carbon levels due to solution treatment and aging were investigated. Ingots of Co-Cr-Mo alloys with three different carbon levels were prepared by vacuum furnace melting; their chemical composition was Co-28Cr-6Mo-xC (x = 0.12, 0.25 and 0.35 mass%). Precipitates were electrolytically extracted from as-cast and heat-treated alloys. An M23C6 type carbide and a phase were detected as precipitates in as-cast Co-28Cr-6Mo-0.12C alloy, and an M23C6 type carbide and an  phase (M6C-M12C type carbide) were detected in as-cast Co-28Cr-6Mo-0.25C and Co-28Cr-6Mo-0.35C alloys. Only the M23C6 type carbide was detected during solution treatment. Complete precipitate dissolution occurred in all the three alloys after solution treatment. The holding time required for complete precipitate dissolution increased with increasing carbon content and decreasing solution treatment temperature. Complete precipitate dissolution occurred in the Co-Cr-Mo-C alloys solution treated at 1523 K for 43.2 ks; they were then subjected to aging from 873 to 1473 K for a heating time up to 44.1 ks after complete precipitate dissolution in solution treatment at 1523 K for 43.2 ks. The M23C6 type carbide with a grain size of 0.1–3 m was observed after aging. A time-temperature-precipitation diagram of the M23C6 type carbide formed in the Co-28Cr-6Mo-0.25C alloy was plotted.



2005 ◽  
Vol 200 (1-4) ◽  
pp. 104-108 ◽  
Author(s):  
S. Mändl ◽  
D. Manova ◽  
H. Neumann ◽  
M.T. Pham ◽  
E. Richter ◽  
...  


DENKI-SEIKO ◽  
1970 ◽  
Vol 41 (4) ◽  
pp. 294-301
Author(s):  
Shôichi Fukui ◽  
Susumu Isobe ◽  
Hiroshi Hirayama


2022 ◽  
Vol 60 (1) ◽  
pp. 83-93
Author(s):  
Young-We Kim ◽  
Yong-Hee Jo ◽  
Yun-Soo Lee ◽  
Hyoung-Wook Kim ◽  
Je-In Lee

The effects of dissolution of the η′ phase by solution treatment on the mechanical properties of A7075-T6 alloy were investigated. Immediately after solution treatment of the T6 sheet at 450 oC or higher, elongation significantly increased and dissolution of the η′ phase occurred. η′ is the main hardening phase. After natural-aging, GPI, which is coherent with the aluminum matrix, was formed and strength increased. When bake hardening after natural-aging was performed, the yield strength slightly increased due to partial dissolution of the GPI and re-precipitation of the η′ phase. In contrast, after solution treatment at 400 oC, there was less elongation increase due to the precipitation of the coarse η phase at grain boundaries and low dissolution of the η′ phase. In addition, when bake hardening after natural-aging was performed, the yield strength decreased due to insufficient GPI, which is the nucleation site of the η′ phase. To promote reprecipitation of the η′ phase, the solution treatment temperature was set to a level that would increase solubility. As a result, the yield strength was significantly increased through re-precipitation of a large number of fine and uniform η′ phase. In addition, to increase the effect of dissolution, a pre-aging treatment was introduced and the bake hardenability can be improved after dissolution.



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