Materials For Extreme Enviornments
Boron-free TiAl complex alloy
The Ti50Al45Nb2.5Mo1.25Ta0.5W0.5V0.25 (TiAl–CA) complex alloy, in comparison to the previously designed TiAl alloys, exhibits a gigapascal-level yield strength (∼1.1 GPa), not only at RT but also at 900 °C, without the addition of any interstitial grain-refining agents during casting. This combination of properties is unusual and difficult to achieve in any metallic system.
The as-cast TiAl CA exhibited a controlled mass gain (1.46 ± 0.07 mg cm⁻²) at 900 °C during 96 hours of isothermal exposure, indicating excellent oxidation resistance. This behavior is attributed to the formation of dense Al₂O₃ and TiO₂ layers on the surface, which effectively limit further oxidation.
Light-weight high entropy superalloy
The Ni-HESA has a lower density (∼7.53 g/cc) and an intricate microstructure comprising Ni₃(Si, Ti)-type γ′ precipitates, annealing twins, and grain size variations within a γ-f.c.c. matrix.
These microstructural features enhance RT work hardenability through back-stress strengthening while ensuring substantial microstructural stability at elevated temperatures, thereby improving both strength and oxidation resistance.
High entropy conventional alloy (HECA) via randomization of matrix
A cost-effective design strategy by introducing configurational randomization (ΔSmix ≥ 1 R) in a compositionally lean f.c.c. matrix to develop a HECA, Ni-12.5Fe-7.5Al-4.75Cr-4.75Mn-0.5Si (at%).
Ni-rich HECA with a lean random matrix was developed, exhibiting superior strength (∼900 MPa), ∼50 % ductility, and enhanced strain hardening compared to conventional Ni-CA and dual-phase Ni-HEA.
Electrochemical tests show improved corrosion resistance (Ecorr: −0.27 ± 0.007 V, and Icorr: ∼1.24 × 10−7 (± 0.2) A/cm2), due to lower galvanic corrosion susceptibility.
Effect of alloying element on properties of complex alloy
Microstructural evolution with increasing V content in Co30Ni45-xVxCr15Fe5Si5 (at. %) alloys shows a transition from a single-phase FCC structure to a multi-phase structure beyond 15 at.% V, while still maintaining good compressive formability (ε > 50%).
Oxide layer thickness and weight gain increase significantly beyond 10 at.% V, with thicker oxide layers (>350 μm) and higher weight gain (>45 mg/cm²) due to the greater reactivity of V with oxygen at elevated temperatures.
Additive Manufacturing
Damage tolerant alloy printing
Damage-tolerant alloys are those that exhibit negligible decrease in mechanical properties despite a high defect content.
Fe38.5Mn20Co20Cr15Si5Cu1.5 (Cu-HEA) is a damage-tolerant alloy because its ductility is approximately 60% that of Fe40Mn20Co20Cr15Si5 (CS-HEA), in spite of having 15 times more defects.
The activation of TRIP at the crack tip has provided Cu-HEA with the ability to delay the crack propagation and thus gave it a damage tolerance.
HEA printing
AM-printed Fe40Mn20Co20Cr15Si5 (CS-HEA) exhibited greater strength due to its high work hardenability, while its substantial uniform ductility is a result of a combination of transformation- and twin-induced plasticity during deformation.
The figure depicts 3D reconstructed X-ray micrograph for CS-HEA showing the defect distribution whereas the BSE image depicts mixed grain morphology having predominantly columnar grains.
Grain boundary architecture
Grain boundary architecture refers to the arrangement and distribution of various structural features along the grain boundaries of a material. These structural features include defects such as vacancies, dislocations, and stacking faults, as well as impurities and segregation of elements
Electron Backscatter Diffraction phase map for as-built Fe40Mn20Co20Cr15Si5 (CS-HEA) doped with 0.5 wt.% B4C (termed CS-BC) as-built CS-BC 120-800 specimens are represented, where the phase fraction of γ-f.c.c. is increased from 26% to 98%. The segregation of B at grain boundary for CS-BC specimen is evident by Energy-dispersive X-ray spectroscopy elemental mapping.
The impact of grain boundary segregation on mechanical properties is shown in tensile stress-strain in comparison with the alloys that are not grain boundary architectured.
Additive overview
Damage-tolerant alloys are those that exhibit negligible decrease in mechanical properties despite a high defect content.
Cu-HEA is a damage-tolerant alloy because its ductility is approximately 60% that of Fe40Mn20Co20Cr15Si5 (CS-HEA), in spite of having 15 times more defects.
The activation of transformation induced plasticity (TRIP) at the crack tip has provided Fe38.5Mn20Co20Cr15Si5Cu1.5 (Cu-HEA) with the ability to delay the crack propagation and thus gave it a damage tolerance.
Non-equiatomic HEAs are designed based on metastability engineering and high entropy approach.
Flexible microstructural evolution in designed HEAs is evident with the variation of Si content.
(E–H) figure shows the microstructural evolution for conventional rolling and (I–K) laser powder bed fusion (LPBF) assisted 3D printing.
Strength ductility synergy in HEA designing
Unexpected strength-ductility synergy was obtained by unconventional phase evolution i.e., γ → ɛ during annealing for Fe39Mn20Co20Cr15Si5Al1 (Al-HEA).
Precipitation of Al and change in martensite morphology played a crucial role in tailoring the strength-ductility synergy.
Corrosion resistance
Microstructural evolution in Fe38.5Mn20Co20Cr15Si5Cu1.5 (Cu-HEA) for D-pass condition, which shows the bimodal microstructural evolution, with very fine grains.
High strength-ductility combination was attained due to controlled transformation induced plasticity effect irrespective of grain sizes
With reduction in grain size, corrosion is found to be slower both thermodynamically and kinetically.
Superplasticity
Super plasticity of as-friction stir processed dual phase-HEAs are shown by the help of engineering stress-engineering strain curves at 700°C with a maximum ductility of 550.
Superplastic flow is maintained due to concurrent occurrence of γ → σ transformation at high temperature
The specimens show diffusional cavitation leading to failure during testing.
Friction Stir Processing
Strength ductility synergy in FSP
The γ-phase dominated HEAs showed slower yet sustained work hardening (WH) rates (~ 2000 MPa) owing to transformation induced plasticity (TRIP) effect whereas ε-phase dominated microstructure showed exceptionally high and sustained work hardening rates (2300–2700 MPa) due to formation of nano-plates or twins in ε-phase upon deformation.
Therefore, MF-HEA design leads to exceptional strength–ductility synergy (1100-1250 MPa, 30-43%) irrespective of the dominance of either γ- or ε-phase in the starting microstructure owing to selective operation of deformation mechanisms in the dominant phase.
Multi pass friction stir processing
FSP was carried out on Fe40Mn20Co20Cr15Si5 (CS-HEA) with overlapping passes of high and low rotational rates for a given transverse speed
Through mechanical testing it is concluded that multi-pass FSP gives good combination of both strength and ductility due to formation of dual phase microstructure.
Fatigue in friction stir processing
The combination of severe plastic deformation and annealing produced a ultrafine grained (UFG) - Cu-HEA with an average grain size of approximately 100 nanometers and an unprecedentedly high fatigue limit, indicating that it could withstand a large number of stress cycles without failing.
This high fatigue limit is supported by the S-N curve, and comparison of fatigue endurance limit vs Ultimate tensile limit.
FSP for conventional alloys
Friction stir processing for enhancing the microstructure and mechanical properties of conventional magnesium alloys, such as the newly designed AXM541 alloy, by means of friction.
The microstructural improvement in Mg-5Al-3.5Ca-1Mn (AXM541) alloy is substantiated by SEM images depicting the refined eutectic particles of nugget after friction stir processing.
The engineering stress-engineering strain curves, true stress-true strain curves, and work hardening curves for AXM541 alloy along the processing direction demonstrate an improvement in mechanical properties.