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Deformation characteristics of Ti–6Al–4V
Materials Science and Technology, 1988AbstractThe deformation characteristics of Ti–6Al–4V have been established by torsion testing in the temperature range 800–1150°C. Constitutive equations are proposed for both the β-region and the α+β-region which, it is suggested, may have some practical applications.
T. Sheppard, J. Norley
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Alloy Digest, 2002
Abstract Carpenter titanium alloy Ti 6Al-4V ELI is a high-purity (extra-low-interstitial) version of Ti 6Al-4V (see Alloy Digest Ti-60, August 2002). The alloy is alpha plus beta and has good biocompatibility. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear ...
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Abstract Carpenter titanium alloy Ti 6Al-4V ELI is a high-purity (extra-low-interstitial) version of Ti 6Al-4V (see Alloy Digest Ti-60, August 2002). The alloy is alpha plus beta and has good biocompatibility. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear ...
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Alloy Digest, 2002
Abstract Carpenter titanium alloy 6Al-4V is an alpha-beta alloy that contains alpha and beta stabilizers and can be heat treated. This alloy accounts for more than 50% of total titanium usage, mostly in aerospace applications. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and ...
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Abstract Carpenter titanium alloy 6Al-4V is an alpha-beta alloy that contains alpha and beta stabilizers and can be heat treated. This alloy accounts for more than 50% of total titanium usage, mostly in aerospace applications. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and ...
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Journal of Alloys and Compounds, 2009
Abstract Air oxidation behaviour of a Ti–6Al–4V alloy was examined over the temperature range of 600–800 °C for different time intervals ranging between 0.5 and 72 h. In addition to the determination of the oxidation kinetics by weight gain measurements, oxygen diffusion zone (ODZ) depth and hardness measurements were conducted on the cross-sections ...
Hasan Guleryuz, Huseyin Cimenoglu
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Abstract Air oxidation behaviour of a Ti–6Al–4V alloy was examined over the temperature range of 600–800 °C for different time intervals ranging between 0.5 and 72 h. In addition to the determination of the oxidation kinetics by weight gain measurements, oxygen diffusion zone (ODZ) depth and hardness measurements were conducted on the cross-sections ...
Hasan Guleryuz, Huseyin Cimenoglu
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Materialwissenschaft und Werkstofftechnik, 1982
AbstractLow‐cycle‐fatigue texts in vacuum and air were performed. Under cyclic loading the Ti‐6Al‐4V showed both cyclic hardening and cyclic softening depending on heat treatment, stress amplitude, and microstructure. Plastic deformation of the β‐phase in the unaged condition due to stress induced martensitic transformation caused cyclic hardening ...
M. A. Däubler, G. Lütjering
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AbstractLow‐cycle‐fatigue texts in vacuum and air were performed. Under cyclic loading the Ti‐6Al‐4V showed both cyclic hardening and cyclic softening depending on heat treatment, stress amplitude, and microstructure. Plastic deformation of the β‐phase in the unaged condition due to stress induced martensitic transformation caused cyclic hardening ...
M. A. Däubler, G. Lütjering
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High-temperature mechanical behavior of Ti-6Al-4V alloy and TiC p /Ti-6Al-4V composite
Metallurgical and Materials Transactions A, 1999Mechanical behaviors at 538 °C, including tensile and creep properties, were investigated for both the Ti-6Al-4V alloy and the Ti-6Al-4V composite reinforced with 10 wt pct TiC particulates fabricated by cold and hot isostatic pressing (CHIP). It was shown that the yield strength (YS) and ultimate tensile strength (UTS) of the composite were greater ...
J. H. Zhu +3 more
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Thermo Physical Property Measurement of Ti-6Al-4V Alloy and Ti-6Al-4V/Nano SiCp Composites
International Review of Mechanical Engineering (IREME), 2014The intention of a thermal-control structure is to sustain all of a spacecraft's components within the permissible temperature limits for all working modes of the vehicle in all of the thermal environments it may be exposed. Metal-matrix composites can endure the tremendous conditions often stumble upon in space environment. The metal-matrix composites
S. Krishna Mohan +2 more
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2020
The 2???3-layer structures, consisting of Ti???6Al???4V alloy and composites on its base with 5...10 % particles of ??i?? or ??i??, were produced by the method of cold pressing and vacuum sintering of multi-component powder mixtures on the base of hydrogenized titanium powder.
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The 2???3-layer structures, consisting of Ti???6Al???4V alloy and composites on its base with 5...10 % particles of ??i?? or ??i??, were produced by the method of cold pressing and vacuum sintering of multi-component powder mixtures on the base of hydrogenized titanium powder.
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Materials Science and Engineering: A, 1997
Abstract Gas-pressure bulge forming of unreinforced Ti-6Al-4V and TiC-reinforced Ti-6Al-4V was performed while cycling the temperature around the allotropic transformation range of the alloy (880–1020 °C). The resulting domes exhibited very large strains to fracture without cavitation, demonstrating for the first time the use of transformation ...
D.C. Dunand, S. Myojin
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Abstract Gas-pressure bulge forming of unreinforced Ti-6Al-4V and TiC-reinforced Ti-6Al-4V was performed while cycling the temperature around the allotropic transformation range of the alloy (880–1020 °C). The resulting domes exhibited very large strains to fracture without cavitation, demonstrating for the first time the use of transformation ...
D.C. Dunand, S. Myojin
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Diffusion Bonding of Ti-6Al-4V Sheet with Ti-6Al-4V Foam for Biomedical Implant Applications
Metallurgical and Materials Transactions B, 2013Advanced metallic bone implants are designed to have a porous surface to improve osseointegration and reduce risks of loosening. An alternative approach to existing surface treatments to create a porous surface is to bond separately produced metallic foams onto the implant.
Brittany Hamilton +3 more
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