scholarly journals Effect of thermal cycling on the cold rolled AISI 316L with varying degree of reduction toward their microstructure and hardness

2021 ◽  
Vol 1034 (1) ◽  
pp. 012164
Author(s):  
Fahmi Mubarok ◽  
Amanda Rosalina
Author(s):  
Hakan Ozaltun ◽  
Samuel J. Miller

This article aims to provide possible mechanical causes for the lowered blister temperatures of RERTR-12 and AFIP-4 fuel plates. Recent experimental investigations to determine the blister threshold temperatures have indicated lower thresholds for similar plates with comparable burn-up histories. Measured blister temperatures of roughly 100 °C lower compared to the previously tested plates may not be satisfactory for some plates. The primary differences between recent experiments and previous tests are: (1) An aggressive cold work process involving large thickness reduction ratios without normalization or full annealing (2) Subjecting the plates to a thermal cycling process prior to irradiation, and finally (3) A primarily frontal neutron flux as opposed to a transverse flux profile. It is believed that the stress field has implications to blister behavior. To investigate this claim, the stress-strain states for the fabrication procedure were evaluated. First, the residual stress profile caused by the cold rolling process was calculated. Modeling of the cold rolling process has shown confirmation of residual stresses of considerable magnitude and the existence of stress gradients with respect to foil thickness prior to the HIP process. Once calculated, these stress profiles were used as an initial condition for the fabrication process. Due to the variation in stress fields depending on location at which a foil is cut from the cold rolled plate, three representative regions were selected and implemented in the HIP simulation. Variation in stresses, depending on location of the cold rolled plate as well and variation in the through-thickness, results in a wide range of mechanical stress states. This suggests that inhomogeneous irradiation and thermal cycling behavior will result from the use of cold rolled foils. Additionally, these results suggest that there will be fundamental differences in fuel plate behavior observed between plates fabricated with cold rolled foils versus hot rolled and fully annealed foils.


2016 ◽  
Vol 66 (5) ◽  
pp. 529 ◽  
Author(s):  
Tarun Nanda ◽  
B. Ravi Kumar ◽  
Vishal Singh

<p>The present work significantly improved the mechanical strength of AISI 316L stainless steel by producing nano-sized grains. Steel was subjected to cold rolling followed by repetitive thermal cycling to produce ultra-fine/ nano-sized grains. The optimum processing parameters including extent of cold deformation, annealing temperature for thermal cycling, soaking period during each thermal cycle, and number of thermal cycles were determined through a systematic step-by-step procedure. After conducting thermal cycling under optimum conditions, a significant amount of grain size reduction was achieved. The effect of nano-sized grains on tensile deformation behavior was analysed. High cold deformation resulted in increased amount of stored strain energy. The stored strain energy accelerated the re-crystallisation kinetics during the thermal cycling process. Every thermal cycle resulted in irregular dispersal of stored energy. This irregular dispersal of stored energy favoured recrystallisation rather than grain growth and led to refinement of grains, in the absence of strain induced martensite. Repetitive thermal cycling promoted grain refinement and resulted in very significant grain size reduction with resultant grain size in the range of 800–1200 nm as compared to initial size of 90–120 μm. The resultant microstructure improved tensile strength by<br />106.8 per cent, from 590 MPa to 1220 MPa.</p>


2020 ◽  
Vol 867 ◽  
pp. 218-223
Author(s):  
Fahmi Mubarok ◽  
Putri Intan Usi Fauzia ◽  
Sutikno ◽  
Ferdiansyah Mahyudin ◽  
Dwikora Novembri Utomo

Investment casting of an orthopedic implant plate based on stainless steel 316L was considered an economical process. Nevertheless, the mechanical properties of the investment casting product were found to be inferior as compared to the implant plate fabricated with other methods such as forging due to their differences in the microstructure. Investment casting mostly produced coarser grain as compared to those with forging or rolled process. In order to improve their mechanical properties, cold-rolling followed by a repetitive thermal cycling process is proposed. The goal is to generate finer grain size through recrystallization process leading to nucleation of new grain during the thermal cycling process thus increasing their strength. Stainless steel 316L was cold-rolled to 52% reduction in thickness and this process generate stored strain energy in the form of dislocation density in the material. The thermal cycling treatment performed within several cycles after cold rolling enabling gradual disperse of stored strain energy that facilitates the recrystallization process that initiates new grain formation. The short holding time within several cycles limits the grain growth that normally occurs during annealing. It was found that thermal cycling treatment at a temperature of 950 °C for 35 seconds within four cycles led to the formation of finer grain size of 22 µm on average as compared to the initial investment casting average grain size of 290 µm. The hardness also increases to 253 HV0.3 in this condition as compared to 155 HV0.3 of investment casting products. Lower thermal cycling temperature than 950 °C during the test did not result in grain refinement thus indicating that strain energy relieves were not enough to aid the recrystallization process.


Metallurgist ◽  
2012 ◽  
Vol 56 (1-2) ◽  
pp. 126-136 ◽  
Author(s):  
I. G. Rodionova ◽  
P. A. Mishnev ◽  
R. R. Adigamov ◽  
Yu. S. Bykova ◽  
S. V. Zhilenko ◽  
...  

Author(s):  
Shiro Fujishiro ◽  
Harold L. Gegel

Ordered-alpha titanium alloys having a DO19 type structure have good potential for high temperature (600°C) applications, due to the thermal stability of the ordered phase and the inherent resistance to recrystallization of these alloys. Five different Ti-Al-Ga alloys consisting of equal atomic percents of aluminum and gallium solute additions up to the stoichiometric composition, Ti3(Al, Ga), were used to study the growth kinetics of the ordered phase and the nature of its interface.The alloys were homogenized in the beta region in a vacuum of about 5×10-7 torr, furnace cooled; reheated in air to 50°C below the alpha transus for hot working. The alloys were subsequently acid cleaned, annealed in vacuo, and cold rolled to about. 050 inch prior to additional homogenization


Author(s):  
H. Lin ◽  
D. P. Pope

During a study of mechanical properties of recrystallized B-free Ni3Al single crystals, regularly spaced parallel traces within individual grains were discovered on the surfaces of thin recrystallized sheets, see Fig. 1. They appeared to be slip traces, but since we could not find similar observations in the literature, a series of experiments was performed to identify them. We will refer to them “traces”, because they contain some, if not all, of the properties of slip traces. A variety of techniques, including the Electron Backscattering Pattern (EBSP) method, was used to ascertain the composition, geometry, and crystallography of these traces. The effect of sample thickness on their formation was also investigated.In summary, these traces on the surface of recrystallized Ni3Al have the following properties:1.The chemistry and crystallographic orientation of the traces are the same as the bulk. No oxides or other second phases were observed.2.The traces are not grooves caused by thermal etching at previous locations of grain boundaries.3.The traces form after recrystallization (because the starting Ni3Al is a single crystal).4.For thicknesses between 50 μm and 720 μm, the density of the traces increases as the sample thickness decreases. Only one set of “protrusion-like” traces is visible in a given grain on the thicker samples, but multiple sets of “cliff-like” traces are visible on the thinner ones (See Fig. 1 and Fig. 2).5.They are linear and parallel to the traces of {111} planes on the surface, see Fig. 3.6.Some of the traces terminate within the interior of the grains, and the rest of them either terminate at or are continuous across grain boundaries. The portion of latter increases with decreasing thickness.7.The grain size decreases with decreasing thickness, the decrease is more pronounced when the grain size is comparable with the thickness, Fig. 4.8.Traces also formed during the recrystallization of cold-rolled polycrystalline Cu thin sheets, Fig. 5.


2018 ◽  
Vol 106 (4) ◽  
pp. 402 ◽  
Author(s):  
Mamoun Fellah ◽  
Linda Aissani ◽  
Alain Iost ◽  
Amel Zairi ◽  
Alex Montagne ◽  
...  

On s’est intéressé dans ce travail à l’analyse du comportement à l’usure et au frottement de deux prothèses totales de hanche en acier AISI 316L et en alliage à base de titane Ti-6Al-7Nb. Les propriétés tribologiques d’usure par glissement sont évaluées à l’aide d’un tribomètre TriboTechnic muni du logiciel tribotester, en accord avec les standards ASTM G 133–95, ISO 7148-1:2012 et ASTMG 99, en présence d’un milieu physiologique (solution de Hank) à une température de 28 à 30 °C. La bille en alumine (Al2O3) a été choisie comme antagoniste. Trois vitesses (1, 6 et 15 mm.s−1) et quatre forces normales (2,4,6 et 10 N) ont été appliquées. Après chaque essai de frottement, l’état de surface a été analysé par un microscope électronique à balayage. Le coefficient de frottement et le volume d’usure étaient plus faibles dans les échantillons testés à une force appliquée de 2 N sous une vitesse de 1 mm.s−1 (0,12 et 0,33) et (0,07 × 107 et 0,09 × 107 μm3) pour l’acier AISI 316L et le Ti-6Al-7Nb, respectivement. Les valeurs du coefficient de frottement obtenues respectent les normes imposées par le domaine du biomédical notamment au niveau de l’état de surface articulaire des prothèses de hanche.


2006 ◽  
Vol 94 ◽  
pp. 477-483 ◽  
Author(s):  
J. Landoulsi ◽  
C. Marconnet ◽  
C. Dagbert ◽  
S. Pulvin ◽  
C. Richard ◽  
...  
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