A5052750898- Material Properties and Applications
- Titanium Alloys Microstructure and Properties
- Metal Forming Simulation Techniques
- Metallurgy and Material Forming
- Engineering Technology and Methodologies
- Engineering and Environmental Studies
- Microstructure and mechanical properties
- Additive Manufacturing Materials and Processes
- Material Properties and Failure Mechanisms
- Radiation Detection and Scintillator Technologies
- High-Velocity Impact and Material Behavior
- Radioactive element chemistry and processing
- Lanthanide and Transition Metal Complexes
- Industrial Engineering and Technologies
- Nuclear Physics and Applications
- Geotechnical and Geomechanical Engineering
- Advanced Welding Techniques Analysis
- Metal and Thin Film Mechanics
- Luminescence Properties of Advanced Materials
- Crystal structures of chemical compounds
- Advanced Surface Polishing Techniques
- Advanced materials and composites
- Engineering Diagnostics and Reliability
- Inorganic Chemistry and Materials
- Organometallic Compounds Synthesis and Characterization
Joint Institute for Nuclear Research
2012-2022
Institute of Metal Superplasticity Problems
2012-2022
Ufa State Petroleum Technological University
2012-2018
Russian Academy of Sciences
1994-2014
Ufa State Aviation Technical University
2014
Institute of Engineering Physics
1993-1995
Moscow Engineering Physics Institute
1993-1995
American Petroleum Institute
1987
Institute of Geology Ufa Scientific Center
1987
Institute of Petroleum Chemistry
1966
A critical analysis of approaches to find constitutive relations from the tests on uniaxial and two axial loading is presented. Then we report methodology fitting parameters for superplastic forming based results cone cup elongated wedge tests. Optimal angles are estimated analytically also finite element simulations. Our comparison experimental numerical simulations corresponding in frame commercial software such as ANSYS10.0 (ED). We carry out different sets chosen relation values friction...
Abstract The superplastic forming process of the VT6 titanium alloy three‐layered hollow structures with goffered filler are investigated. Based on results experimental studies and finite element modeling, we determine rational parameters such as gas pressure increase rate, when flow condition is satisfied for ribs, processing time minimal.
A method is proposed which allows one to search for a solution inverse problems of identifying constitutive relations from the results technological experiments. The uses simplified mathematical models plastic metal forming processes based on membrane theory shells, calculations material constants K and m entering Backofen’s relation superplasticity experiments carried out directly equipment. differs others by fact that its implementation only two test formings hemispherical domes at...
Application of the conventional superplasticity (SP) allows producing unique hollow structures. One remarkable example is titanium blade air engine fan produced by Rolls-Royce. However, high temperature Ti-6Al-4V alloy processing (~ 927 °С) limits wide industrial application SP. On base experimental data examples superplastic forming (SPF) structures for aerospace out ultrafine-grained (UFG) VT6 (Ti-6Al-4V) using an effect low SP are demonstrated. We used two-phase in VSMPO, Verhnyaya Salda,...
Application of the conventional superplasticity (SP) allows producing unique hollow structures. One remarkable example is titanium blade air engine fan produced by Rolls-Royce. However, high temperature alloys processing (~ 927 °С) limits wide industrial application SP. The solution mentioned issue can be found through low-temperature Ti-6Al-4V alloy with ultrafine grain structure at range 600 800 °С has enough ductility resources for superplastic forming (SPF) parts complicated shape....
In the present work, process of superplastic forming hemispherical shells from blanks different profiles on basis computer modeling is considered. A relevant task in to reduce thickness difference, which will significantly improve quality their geometric characteristics with a general reduction cost production. It shown that shell billet constant fixed flange leads an inevitable appearance differenses. has been number works that, case made titanium alloys, difference exceeds 50 %. Various...
Проведены результаты экспериментов по сварке давлением титанового сплава ВТ6 в условиях низкотемпературной сверхпластичности. Показано, что чем ниже температура, тем выше должно быть значение давления относительно напряжения течения при этой температуре. При этом качество твердофазного соединения существенно зависит от степени деформации.
The mechanical behavior at shock loading of samples from titanium alloy VT6 with different structural: coarse-crystalline lamellar morphology phases (CC), microcrystalline globular (MC), nanostructure (NS) is analyses. Results tests showed that in the CC and MC structures have higher level impact toughness comparison nanostructure. With reduction size structural components work crack nucleation raises on % 55, propagation reduces 70. Impact decreases 20. picture fracture reflects...
Uniaxial tension and superplastic forming experiments are performed with ultra fine grained titanium VT6 alloy under conditions of low temperature superplasticity at temperatures 600 650оС. The initial mean grain size in was 0,2 mm. Pores were not display the steady state up to 600% sample extension. It is revealed accelerated a b-phase growth stimulated by deformation.<br /> Ключевые слова: Низкотемпературная сверхпластичность, поры, сверхпластическая формовка, титановый сплав ВТ6.<br <br
Corrugated core panels manufactured by methods of superplastic forming concurrent with diffusion bonding (SPF/DB) are promising for the production high specific strength articles. One serious problems arising in corrugated is concerned formation outer folds. The cause folding uneven deformation skin sheets. In this study, process a panel from titanium alloy VT6 (analogue Ti-6Al-4V) computer simulation considered. Finite element modeling carrying out using ANSYS software. formulation boundary...