Various studies have been conducted to investigate the influence of microstructure on the mechanical properties of Ti6Al4V alloys. The results show that changes in microstructure can cause an increase in tensile strain. Various sintering techniques and thermal treatments have been proposed to control the microstructure. This study focuses on a novel thermomechanical processing method to produce equiaxed ultrafine grains in Ti-6Al-4V alloy.
In addition to the a-Ti grain size, the amount of high angle grain boundaries was also increased. The microstructure of Ti-6Al-4V alloy was investigated using optical microscopy and scanning electron microscopy. The results show that the a + b lamellar microstructure exists in perpendicular form. The microstructure evolves in a dynamic manner. This results in a continuous recrystallization.
The results indicate that the b phase is thinner than the a phase. The volume fraction of the b phase is also relatively low. This results in an increase in hardness. The a' phase is acicular and martensitic. The a-Widmanstatten laths are commonly observed in wrought components. The a + b lamellar is composed of an acicular martensite phase and a perpendicular a-lamellar phase. The thickness of the a-lamellae and the length of the a-Widmanstatten grains decreased with increasing cooling rates.
The results show that the microstructure of the LPBF Ti6Al4V alloy is martensitic. However, the microstructure of the AC-TC4 alloy is not detected from the center to the periphery of the alloy. This results in a coarse lamellar microstructure of a-Ti grains, which causes a reduction in the yield strength.
Several studies have focused on the correlations between microstructure and tensile properties of Ti6Al4V. These correlations are often non-linear and it is difficult to make a definitive conclusion. However, the study of these correlations is important to understand how to optimize performance in the future.
The largest tensile strength was achieved by a sample with an offset of 0.28 mm. In general, smaller offsets increase yield strength. However, the ultimate tensile strength is inversely proportional to the lath width.
The ultimate tensile strength of a weldment is slightly higher than the parent metal. The yield stress of the weldment is 5% lower than the parent metal. This indicates that the weldment has less area than the parent metal.
The microstructure of Ti6Al4V is complex and depends on several factors. The tensile properties of a fabricated Ti-6Al-4V alloy are mainly affected by the grain size of the b grains. Generally, the grain size perpendicular to the tensile direction is about 1-4 mm. However, determining the exact size of b grains is not possible.
The microstructure of Ti-6Al-4V samples is characterized by the presence of layered structure, which is formed during welding. This layered structure is evident in the surface of the components. It also appears in the microstructure of specimens with higher energy input.
The microstructure of tensile specimens shows the presence of dimples, which are indicative of the alloy's plastic deformation at a low temperature. These dimples are also a good sign of the alloy's ability to deform plastically under cryogenic conditions.
Several studies have been conducted to evaluate the corrosion resistance of Ti6Al4V titanium alloy. It is used in many industries. This alloy has high strength-to-weight ratios and corrosion resistance. It is commonly used in medical devices and aerospace applications.
Several electrochemical techniques were used in this study. These include electrochemical impedance spectroscopy (EIS) and potentiodynamic polarization curves. The results obtained can be used by engineers in developing processes for Ti6Al4V alloy.
The Ipas value was reported to be 3.5 mA/cm2 in Hank's solution. The polarization resistance value was obtained by oxidizing the alloy during three hours. This value was higher than that of the specimen oxidized during one hour.
This value indicates that the electrode surface is active. This effect is caused by the formation of protective oxide layers. This oxide layer will decrease the release of V ions.
The Ecorr value indicates that the alloy has a tendency to increase its corrosion resistance. This value was monitored with a potentiostat. The value was not affected by the oxidation time.
The passive current density value was similar to that of the Ipas value. This value was measured with an ACM Instruments potentiostat. It was given 20 minutes to stabilize. The resistance value remained stable for 72 days.
The best corrosion performance was achieved by plasma-oxidizing the alloy at 600 degC for three hours. This resulted in the lowest passive and corrosion current density.
Increasing the abrasion resistance of titanium alloys is a major challenge. The main wear mechanisms are abrasion and fatigue. However, low abrasion resistance is especially noticeable in femoral components. Several efforts have been made to improve the abrasion resistance of titanium alloys. Some methods involve ion implantation, surface functionalization, or coating. However, the most effective method is to modify the alloy by adding diazonium salts.
Using diazonium salts, an evenly distributed aryl layer was produced. The coating was prepared on the surface of Ti6Al4V alloy by combining plasma diffusion and magnetron sputtering. The coating was analyzed by X-ray diffraction and scanning electron microscopy. The wear resistance of the composite coating was tested using an abrasion tester. The specific wear rate decreased by 52%.
Polyurethane layers are attached to the modified alloy to improve the abrasion resistance of the coated surface. The protective layer should be evenly distributed over the alloy surface to affect the properties of both the coated surface and the alloy in an equal manner. The polyurethane layer can be of different thickness.
The polyurethane layer on the modified alloy had a lower coefficient of friction than the unmodified alloy. The maximum coefficient of friction was 0.8 for the untreated alloy. In the nitrided alloy, the coefficient of friction was reduced by 64%. The specific wear rate decreased by double that of the untreated alloy.
Several studies have been conducted on microcracks in Ti-6Al-4V alloy. This alloy has been widely used in aerospace and biomedical industries. Its good mechanical properties have made it a design choice for various applications. However, its poor plastic deformability makes it difficult to manufacture parts at room temperature. This study aims to improve the plastic deformability of Ti-6Al-4V alloy. It also studies the deformation mechanism with electropulsing and conventional thermal treatment.
The EDM-treated surface of Ti-6Al-4V alloy showed some surface microcracks. This was due to the application of a pulsed current in the EDC process. The pulsed current improved the plastic deformability of the alloy and reduced the deformation resistance.
An electro-probe microanalyzer was used to study the distribution of alloying elements in the micro-crack. The crack fronts were characterized with a-Ti phase and b-Nb phase. The b-Nb phase was uniformly distributed in the a-Ti matrix. However, the a-Ti phase was only visible at a higher magnification.
A hat-shaped specimen was prepared for metallographic analysis. It was axially sectioned into an upper hat part, lower brim part and shear zone. The brim part was divided into a shear zone and a non-shear zone. Compared with the shear zone, the brim part was observed to have a microcrack.
The lower brim part of the specimen was drilled through in order to investigate the microcrack propagation. In addition, the axial section was examined to identify the microstructure of the specimen. It was found that the microcracks were present only when the TiC mass percent exceeded 40 wt.%.
Various studies have been carried out on the effect of heat treatment on the mechanical properties of Ti6Al4v alloy. The heat treatment of L-PBF-manufactured Ti6Al4v parts play a crucial role in improving mechanical properties. However, the effect of heat treatment on the microstructure of Ti6Al4v alloy has not been fully studied. This paper aims to investigate the effect of heat treatment on the microstructure and properties of L-PBF-manufactured Titanium alloy parts.
In this study, the effect of heat treatment on the microstructure, tensile properties and fatigue properties of Ti6Al4v alloys is investigated. The mechanical properties of the alloy are directly dependent on the microstructure. The effects of defects on the mechanical properties of the alloy are also discussed critically.
In order to investigate the effect of heat treatment on the mechanical properties, high-temperature tests were carried out. Stress-strain curves were obtained. The J-C constitutive model was also derived from the data. The model was fitted to the data to establish the material constants.
The results show that the microstructure of the alloy shows a gradual increase in plastic strain with increasing temperature. In addition, the area fraction of the a' phase increases as the temperature increases. The a' phase is a close packed hexagonal structure. In addition, the intermetallic compound layer is decreased. The oxidative wear dominates at higher temperatures. However, the results do not show any significant difference when stress-relieving heat treatment was performed.
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