V.A. Vorontsov

ORCID: 0000-0002-1958-0602
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About
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Research Areas
  • High Temperature Alloys and Creep
  • Intermetallics and Advanced Alloy Properties
  • Titanium Alloys Microstructure and Properties
  • Advanced Materials Characterization Techniques
  • Nuclear Materials and Properties
  • Hydrogen embrittlement and corrosion behaviors in metals
  • Microstructure and Mechanical Properties of Steels
  • Aluminum Alloy Microstructure Properties
  • Metal Alloys Wear and Properties
  • High-Temperature Coating Behaviors
  • Microstructure and mechanical properties
  • Metallurgy and Material Forming
  • Material Properties and Applications
  • Metal and Thin Film Mechanics
  • Advanced materials and composites
  • Advanced ceramic materials synthesis
  • High Entropy Alloys Studies
  • Advanced Theoretical and Applied Studies in Material Sciences and Geometry
  • Fiber-reinforced polymer composites
  • Advanced Surface Polishing Techniques
  • Copper Interconnects and Reliability
  • Magnetic and transport properties of perovskites and related materials
  • Orthopaedic implants and arthroplasty
  • Catalysts for Methane Reforming
  • Shape Memory Alloy Transformations

University of Strathclyde
2019-2024

NIIGrafit
2014-2024

Imperial College London
2012-2022

Rosatom (Russia)
2017

University of Cambridge
2009-2014

Novosibirsk State Technical University
2013

Purdue University West Lafayette
2005

A polycrystalline hot working ingot metallurgy processing route for γ/γ′ Co–Al–W superalloys has been developed. Based on Co–7Al–7W (at%), substitutions of Mo, V, Ti, Ta, Ni, Si, Fe and Cr were examined. The γ′ solvus was found to follow the same trends as those exhibited by alloys with higher fractions considered other investigators. Excessive additions lead discontinuous coarsening eventually, loss phase from microstructures observed. Ni examined, some success, restore raise temperature....

10.1016/j.intermet.2013.10.022 article EN cc-by-nc-nd Intermetallics 2013-11-21

The lattice misfit and diffraction elastic constants in hot rolled polycrystalline Co–7Al–5W–2Ta Co–6Al–6W–2Ti (at.%) are measured using neutron synchrotron X-ray diffraction. the two alloys was found to be +0.67 +0.59%, at HRPD. increase with temperature, as Ni superalloys. This implies that amount of coherency strengthening increases temperature. show γ′ phase is less stiff than γ matrix all orientations, which means load shedding will occur phase.

10.1016/j.msea.2014.05.044 article EN cc-by Materials Science and Engineering A 2014-05-22

10.1016/j.msea.2013.09.081 article EN Materials Science and Engineering A 2013-10-07

A steel with nominal composition Fe-28Mn-8Al-1.0C in mass percent was hot rolled at two temperatures, 1100 °C and 850 subsequently aged 550 for 24 h. The lower temperature rolling resulted a yield strength increment of 299 MPa while still retaining an elongation to failure 26%. large improvement attributed increase residual dislocation density which retained even after the ageing heat treatment. homogeneous precipitation κ-carbides both samples also showed that high did not adversely affect...

10.1016/j.scriptamat.2022.114626 article EN cc-by Scripta Materialia 2022-02-24

An extended phase field model of dislocations in Ni-base superalloys is presented. It incorporates the recently developed effective γ-surfaces for both matrix and precipitate phases, obtained from atomistic simulations. These novel feature extrinsic stacking faults as additional local minima. Thus, they offer an increased number available dislocation dissociation pathways within system. The new has been used to simulate a variety mechanisms γ′ shearing proposed literature. A critical...

10.1080/14786435.2011.630691 article EN The Philosophical Magazine A Journal of Theoretical Experimental and Applied Physics 2011-12-07

A SiC reinforced Ti‐5Al‐5Mo‐5V‐3Cr matrix metal composite is developed. Monolithic blocks of alloy are hot rolled via pack rolling to produce foils for MMC panel fabrication. These consolidated using isostatic pressing and solution treated aged optimum strength. The panels exhibited a strength 2 GPa in tension 3.5 compression, compared the aerospace steel 300M, which has tensile 1.69 GPa. fatigue performance material exceeded that MMCs developed Ti‐21S or Ti‐6Al‐4V matrices. Finally,...

10.1002/adem.201700027 article EN Advanced Engineering Materials 2017-03-22
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