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        1 - The Effect of Magnesium on the Microstructure and Stress Rupture Properties of Hastelloy X Supealloy
        Masumeh seifollahi Afagh panahi moghaddam seysd Mahdi Abbasi seyed Mahdi ghazi mir saeed
        In the present study, the effects of magnesium on the microstructural characteristics and stress-rupture properties of the Hastelloy X superalloy were investigated. In this regard, four alloys with different amounts of magnesium (0, 17, 33, 47 ppm) were cast via the vac More
        In the present study, the effects of magnesium on the microstructural characteristics and stress-rupture properties of the Hastelloy X superalloy were investigated. In this regard, four alloys with different amounts of magnesium (0, 17, 33, 47 ppm) were cast via the vacuum induction melting and then purified via the electro slag remelting. Microstructural observations were carried out through optical and scanning electron microscopes, and phase analysis was performed by X-ray diffraction. The stress rupture test was carried out at 815 °C/130 MPa. The results showed an almost significant effect of magnesium on decreasing grain size and sulfur content and increasing M6C carbides volume fraction. Magnesium changed the morphology of carbides from the course and continue to finely divide one. Mg segregated at the grain and carbide boundary decreases the lattice parameters of the matrix and changes the composition of M6C. Magnesium increased the rupture life by 46%. The most important causes for improving the rupture life of the Hastelloy X in the presence of magnesium are the increasing carbides volume fraction, improving its morphology, and decreasing sulfur content. Manuscript profile
      • Open Access Article

        2 - Investigating the Effects of Boron and Zirconium on the High-Temperature Fatigue Behavior of Nimonic 105 Super Alloy
        Zahra Asghary Masumeh Seifollahi Maryam Morakabati Seyed Mahdi Abbasi
        This study investigates the low-cycle fatigue of Nimonic105 alloy with boron and zirconium of 0.003-0.013 wt.% and 0.0-0.16 wt.%, respectively at 750 °C. The fatigue test results indicated that the alloy with boron of 0.013 wt.% had the highest fatigue life of 400 c More
        This study investigates the low-cycle fatigue of Nimonic105 alloy with boron and zirconium of 0.003-0.013 wt.% and 0.0-0.16 wt.%, respectively at 750 °C. The fatigue test results indicated that the alloy with boron of 0.013 wt.% had the highest fatigue life of 400 cycles, while the base alloy showed the lowest fatigue life of 21 cycles at 2% strain amplitudes. For the alloy with 0.16 wt.% Zr, and the alloy with 0.08 wt.% Zr and 0.006 wt.% B, cyclic-hardening occurred at a constant slope. Then, hardening followed a nonlinear procedure at a reducing rate. Finally, softening and fracture happened. For 0.013 wt.% Zr alloy, however, the diagram reached a stable state or slow cyclic-softening and failed after a relatively short period of cyclic -softening. The Coffin-Manson equations’ parameters verified the increased flexibility due to the addition of B. to be a factor in improving high-temperature LCF strength. The investigation of the samples’ fracture surfaces indicated that the intergranular fracture of the base alloy with the lowest fatigue life became intergranular and transgranular fracture in the alloy with 0.16 ‌wt.% Zr content and the alloy with 0.08 wt.% Zr content and 0.006 wt.% B contents. Also, 0.013 wt.% B alloy with the highest fatigue life showed a completely transgranular fracture. Manuscript profile
      • Open Access Article

        3 - Influence of Withdrawal Rate on As-Cast Microstructure and Stress-Rupture Life of Directionally Solidified Rene80 Superalloy
        sobhan Rajabi nejad Masumeh seifollahi seyed mahdi Abbasi Seyed Mahdi Ghazi mirsaeed
        The purpose of this study is to investigate the effects of withdrawal rate on the dendrite microstructure and its formation mechanism, the porosity, and the interaction between them in Rene 80 superalloy. So, Rene 80 Ni-base superalloy was directionally solidified on a More
        The purpose of this study is to investigate the effects of withdrawal rate on the dendrite microstructure and its formation mechanism, the porosity, and the interaction between them in Rene 80 superalloy. So, Rene 80 Ni-base superalloy was directionally solidified on a laboratory scale using the Bridgman method. The cylindrical rods were grown at withdrawal rates of 2, 4, 6, 8, and 10 mm.min-1. Dendritic structure and solidification microporosities were evaluated in transverse and longitude sections. The results showed that when the withdrawal rate was increased, the primary and secondary dendritic arm spacing decreased. With an increasing withdrawal rate, which causes to decrease in the dendritic arms spacing, the volume fraction of inter-dendritic gamma prime was first decreased until the rate of 6 mm.min-1, and after that, its volume fraction increased. This structure results from peritectic and eutectic transformations with checkerboard-like and fan-like morphology, respectively. Moreover, the volume fraction of microporosities was minimal at the rate of 6 mm.min-1, while their average size decreased from 13.2 to 8.7 μm. The specimens were given a two-stage heat treatment followed by a stress rupture test at 191 MPa and 980˚C. It was shown that at R=6 mm.min-1, directionally solidified rods with a less solidification microporosity and well-orientated dendritic structure give higher rupture life of 25.43 hrs. Manuscript profile