Authors: M.R. Shagiev, R.M. Galeyev, Oleg R. Valiakhmetov, Rinat V. Safiullin
Abstract: Mechanical properties of a Ti2AlNb-based intermetallic alloy both at room and elevated temperatures were considerably improved due to formation of a homogeneous microstructure with the average grain size of about 300 nm. At room temperature, elongations up to 25% were obtained and the ultimate strength reached 1400 MPa. The alloy exhibited superplastic behavior in the temperature range of 850-1000°C. The maximum elongation of 930% and steady state flow stress 50 of about 125 MPa were obtained at 900°C and strain rate of 4.210-3 s-1. The nanostructured material was used for production of intermetallic sheets and multilayer composite plates consisting of alternating layers of orthorhombic intermetallic and commercial high temperature titanium alloy. Ti2AlNb-based sheets and composites exhibited improved mechanical properties.
105
Authors: M.R. Shagiev, G.A. Salishchev
Abstract: Homogeneous nanocrystalline structure with the average grain size of about 300 nm was
produced in Ti2AlNb-based intermetallic alloy by a thermomechanical processing which included
multistep isothermal forging at temperatures below the β-transus and intermediate annealings.
Nanostructured material possessed excellent mechanical properties. At room temperature,
elongations up to 25% were obtained and the ultimate strength reached 1400 MPa. The alloy
exhibited superplastic behavior in the temperature range of 850-1000°C. The maximum elongation
of 930% and steady state flow stress σ50 of about 125 MPa were obtained at 900°C and strain rate of
4.2×10-3 s-1. The rolling temperatures of nanostructured alloy were defined from analysis of its
mechanical behavior at a typical rolling strain rate of about 10-1 s-1 and intermetallic sheets with
improved mechanical properties were produced.
153
Authors: M.H. Parsa, H. Davari, A.M. Hadian, Mahmoud Nili-Ahmadabadi
Abstract: Hybrid Rotary Friction Welding is a modified type of common rotary friction welding processes. In
this welding method, parameters such as pressure, angular velocity and time of welding control
temperature, stress, strain and their variations which play an important rule in defining optimum
process parameter combinations in order to improve the design and manufacturing of welding
machines and quality of welded parts. Thermo-mechanical simulation of friction welding has been
carried out. It has been shown that simulation is an important tool for prediction of generated heat
and strain at the weld interface and can be used for prediction of microstructure and evaluation of
quality of welds. For simulation of Hybrid Rotary Friction Welding a commercial finite element
program has been used and the effects of pressure on temperature and strain variations have been
investigated.
287
Authors: D.A. Chinakhov, E.P. Agrenich
833
Authors: M.J. Thomas, Bradley P. Wynne, Eric J. Palmiere, Ken P. Mingard, Bryan Roebuck
Abstract: An assessment of the inhomogeneity of microstructure generated within plane strain
compression test specimens has been performed using the nickel based superalloy, Waspaloy. Two
variables were investigated: the effect of strain rate and the effect of friction at the tool/specimen
interface. Tests were performed at 1040°C at nominal strain rates of 0.01 and 1 s-1 with and without
a glass based lubricant. At the low strain rate the microstructure was relatively homogeneous
regardless of the friction conditions. At the high strain rate there was significant microstructure
variation from surface to mid plane which was further exaggerated by increased friction.
Quantification of the inhomogeneity, however, is non-trivial in this alloy due to the complicated
recrystallisation behaviour it exhibits and difficulty in differentiating between recrystallised and
non-recrystallised grains.
589
Authors: Satoru Kobayashi, Stefan Zaefferer
Abstract: A fine grained and recovered structure with densely formed fine particles has been created
by means of a thermomechanical process (TMP) in Fe3Al (bcc derivative structure)-based alloys. The
TMP consists of the following two parts; the first part is grain refinement and the second the creation
of recovered structure stabilized by fine particles. It was found in the first part that coarse particles are
required in the process of deformation to refine grain size by particle stimulated nucleation (PSN)
mechanism. Fine M2C type carbide particles were densely precipitated in the second part. These
particles were observed to inhibit the growth of subgrains formed around coarse particles during
annealing at 700°C. This result suggests that if the fine particle density remains high, the recovered
structure can be maintained at 700°C.
235
Authors: Han Sol Kim, Tae Yeub Ra, H.J. Bang, Young Gyu Yoo, Won Yong Kim
Abstract: Microstructure and texture of Ti-Nb-Si based alloys, prepared by water quenching from
β-phase field, cold rolling and recrystallization heat treatment followed by water quenching, were
investigated in terms of optical microstructure and analysis of X-ray pole figure result. Optical
microstructure observation and X-ray diffraction analysis revealed that the microstructure of
as-quenched sample appeared to mixture appearance consisting of mostly bcc-structured β phase and
small amount of orthorhombic-structured α″ phase. After cold rolling elongated structure parallel to
the rolling direction was observed, and equiaxed structure with the average grain size of about
20~30μm was developed for the sample after recrystallization heat treatment. In as-cold rolled sample
we have found well-developed α-fiber texture components which are frequently observed in
bcc-structured metals and alloys. In recrystallized sample, rotated cube texture component was
weakly detected. The variation of elastic modulus values was interpreted in terms of changes in
texture components depending on thermomechanical processing.
789
Authors: Martin Riedler, Martin Stockinger, Michael Stoschka, Wilfried Eichlseder
Abstract: With the objective of creating a simulation model for the lifetime calculation of
forged aerospace components it is necessary to clarify the damage mechanisms in the
materials used. This has been researched for the Ni-base alloy Inconel 718 by varying the
forging parameter effective plastic strain rate, which is realised by using three types of
equipment: hydraulic press, screw press and hammer. Specimens processed at the screw press
show the highest lifetime by keeping all other forging parameters unvaried. Micro structural
investigations show that the amount and morphology of dominant as-large-as grains play a
important role. This methodology is currently investigated for Ti-6Al-4V. Lifetime tests show
that besides effective strain and anisotropy the influence of morphology is important. As soon
as the model status allows lifetime analyses the thermo-mechanical process (forging and heat
treatment) can be developed depending on the desired lifetime specifications in order to
realise an interdisciplinary lifetime optimisation of forgings. A further aim is the use of basic
coherences of safe-life and fail-safe approaches in the low and high cycle fatigue region in
order to reasonable handle with flaws and defects at the edge layer.
185
Authors: Kemal Delijić, V. Asanović, Dragan Radonjić
Abstract: The paper deals with the effects of thermo-mechanical processing parameters on the
properties of two Al-Fe-Si foil alloys. Two twin roll cast alloys with high Fe/Si ratios (Fe/Si≈6)
were processed under different combinations of homogenization, deformation and annealing
treatments. The influence of small additions of manganese on the mechanical behavior and plastic
anisotropy of sheets in hardening and annealing conditions are described. The corrosion resistance
of tested sheets in chloride ambience is also presented, because this type of Al foils is dominantly
used in the packaging (food) industry and heat exchangers.
559
Authors: Y. Song, M.D.J. Cross, W. Mark Rainforth, Bradley P. Wynne
Abstract: The effect of interpass time during thermomechanical processing of AA61111 on flow
behaviour and microstructure evolution has been investigated. This was achieved using plane strain
compression testing undertaken on the Sheffield thermomechanical compression (TMC) facility,
using the hit-hold-hit-quench approach. Following solution treatment at 560°C for 1200s, samples
were water mist quenched to 320°C and deformed at a constant strain rate of 85s-1 to an initial strain
of 0.5, unloaded and held for delay times of 0.019, 6, 60, 600 and 6000s and then given a second
deformation for a further strain of 0.5, followed by a water quench to room temperature. Hardening
of the alloy was observed, the extent of which was dependent on the hold time. The microstructure
of the samples was quantified by TEM in order to determine the extent of strain induced
precipitation. TEM identified precipitation, predominantly β and Q phases, on dislocation lines, the
size and volume fraction of which were a function of the hold time. The coarsening rate during the
hold period of the precipitates was considerably faster than for coarsening following a conventional
precipitation treatment. The size of the microband structure at the end of the double deformation
was a function of the hold time, suggesting that coarsening of the precipitates during the hold had
altered the Zener pinning potential. The implication of these observations on the thermomechanical
processing of 6xxx alloys is discussed.
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