Laser beam welding of a Ti-15mo/TIB metal-matrix composite

A Ti-15Mo/TiB metal-matrix composite was produced by spark plasma sintering at 1400 °C. The fractions of the elements in the initial powder mixture were 80.75 wt.% Ti, 14.25 wt.% Mo, and 5 wt.% TiB2. The initial structure of the synthesized composite was composed of bcc titanium matrix and needle-like TiB reinforcements with an average thickness of 500 ∓ 300 n

Effect of hot rolling on the microstructure and mechanical properties of a Ti-15Mo/TiB metal-matrix composite

A Ti-15Mo/TiB metal matrix composite was produced by the spark plasma sintering process at 1400 °C using a Ti-14.25 wt.% Mo-5 wt.% TiB2 powder mixture. The microstructure and mechanical properties of the composite were studied after non-isothermal rolling of specimens heated to 1000 °C to a thickness strain of ~0.

Effect of hot rolling on the microstructure and mechanical properties of a Ti-15Mo/TiB metal-matrix composite

A Ti-15Mo/TiB metal matrix composite was produced by the spark plasma sintering process at 1400°C using a Ti-14.25 wt.% Mo-5 wt.% TiB2 powder mixture. The microstructure and mechanical properties of the composite were studied after non-isothermal rolling of specimens heated to 1000°C to a thickness strain of ~0.7. Transmission and scanning electron microscopy, as well as X-ray analysis were used for microstructure examinatio

Effect of Hot Rolling on Microstructure and Mechanical Properties of a Ti–15 %Mo/TiB Metal–Matrix Composite

A Ti–15Mo/TiB metal-matrix composite was obtained by the spark plasma sintering at 1400 °C; a powder mixture of Ti-14,25 (wt.) % Mo-5 (wt.) % TiB2 was used. The microstructure and mechanical properties of the composite were studied after rolling samples heated to 1000 °C to a total true strain of ~ 0,7. It was found the rolling led to considerable increase in ductility without a significant loss of strength of the composite.Металл-матричный композит Ti-15Mo/TiB был получен искровым плазменным спеканием порошковой смеси Ti — 14,25 вес. %Mo — 5 вес. % TiB2 при 1400 °C. Микроструктура и механические свойства композита были изучены после горячей прокатки при 1000 °C до истинной деформации ~0,7. Показано, что прокатка привела к значительному повышению пластичности композита без существенной потери прочностных характеристик

Effect of Deformation and Annealing on the Structure and Mechanical Properties of Medium Entropy Alloy Fe65 (CoNi)25Cr9.5C0.5

Исследованы структура и механические свойства при комнатной и криогенной температурах нового среднеэнтропийного сплава Fе65(CoNi)25Cr9,5C0,5 в литом, деформированном и отожженном состояниях. Деформация осуществлялась путем холодной прокатки до 80% обжатия. Последующий отжиг привел к выделению карбидов типа M23C6.Structure and mechanical properties at room and cryogenic temperatures of a new medium-entropy Fе65 (CoNi)25Cr9.5C0.5 alloy were investigated in the as-cast, cold-worked, and annealed conditions. Deformation was carried out by cold rolling up to 80% reduction. Subsequent annealing resulted in the precipitation of M23C6 type carbides.Работа выполнена при финансовой поддержке Российского научного фонда, грант № 20-79-10093. Авторы благодарны Центру коллективного пользования «Технологии и материалы НИУ „БелГУ“» за помощь.The work was carried out with the financial support of the Russian science foundation, grant No. 20–79–10093. The authors are grateful to the center for collective use “Technologies and materials of nru ‘Belsu’” for their help