Mechanical Properties | Metric | English | Comments |
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Tensile Strength, Yield | >= 828 MPa | >= 120000 psi | 0.2% proof |
Kobe Steel KS EL-F Alpha-Beta Titanium Alloy, Annealed Nominal Composition: Ti-4.5 Al-4 Cr-0.5 Fe-0.2 C Applications: Aircraft parts, connecting rods, valve spring retainers, structural parts, golf club heads.Features:High strength, excellent balance b.. |
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Tensile Strength, Yield | >= 828 MPa | >= 120000 psi | 0.2% proof |
Kobe Steel KS6-4 Alpha-Beta Titanium Alloy, ASTM Gr. 5, Annealed Nominal Composition: Ti-6 Al-4 V Applications: Aircraft parts, connecting rods, valve spring retainers, structural parts, golf club heads.Features:High strength, excellent balance between strength .. |
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Tensile Strength, Yield | >= 828 MPa | >= 120000 psi | 0.2% proof |
Kobe Steel KSTI-9 Alpha-Beta Titanium Alloy, ASTM Gr. 35, Annealed (coil, sheets) Nominal Composition: Ti-4.5 Al-2 Mo-1.6 V-0.5 Fe-0.3 Si-0.03 C Applications: Aircraft parts, connecting rods, valve spring retainers, structural parts, golf club heads.Features:High strength, excel.. |
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Tensile Strength, Yield | >= 828 MPa @Strain 0.200 % |
>= 120000 psi @Strain 0.200 % |
Longitudinal |
TIMET 6-4 Titanium Alloy (Ti-6Al-4V; ASTM Grade 5) Rod or Thickness, Medium To High Strength General-Purpose Alloy. Minimum tensile property data below are specific to Rod or Thickness, |
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Tensile Strength, Yield | >= 828 MPa @Strain 0.200 % |
>= 120000 psi @Strain 0.200 % |
L and LT Directions |
TIMET 6-4 Titanium Alloy (Ti-6Al-4V; ASTM Grade 5) Sheet and Plate, 0.025-1.000 in, Annealed, Per ASTM B265 Medium To High Strength General-Purpose Alloy. Minimum tensile property data below are specific to Sheet and Plate, 0.025-1.000 in, Annealed, Per ASTM B265; other specific form/thickness entries a.. |
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Tensile Strength, Yield | 828 MPa @Strain 0.200 % |
120000 psi @Strain 0.200 % |
Typical |
TIMET 6-4 Titanium Alloy (Ti-6Al-4V-0.1Ru; ASTM Grade 29) Medium To High Strength General-Purpose Alloy. Property data below are typical of Timet® 6-4 ELI (without Ru). The 0.1 Ru ELI variant is used for enhanced corrosion resistance.Data provided by TI.. |
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Tensile Strength, Yield | 828 MPa @Strain 0.200 % |
120000 psi @Strain 0.200 % |
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ATI Allegheny Ludlum Grade 5 Titanium 6Al-4V (UNS R56400) Uses: blades, discs, rings, airframe, fasteners, components, vessels, cases, hubs, forgings.Mechanical property data below is typical of annealed samples at room temperature.Information provided by .. |
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Tensile Strength, Yield | 828 MPa @Strain 0.200 % |
120000 psi @Strain 0.200 % |
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ATI Allvac® Vasco® 422 Specialty Steel, Heat Treatment: 1038°C (1900°F) Anneal Data provided by Allvac.Applications: Jet engine parts, brackets, disks, bolts, blades fasteners, aircraft components. Parts for steam and gas turbines, engines. |
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Tensile Strength, Yield | 828 MPa @Strain 0.200 % |
120000 psi @Strain 0.200 % |
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ATI Allvac® 520 Nickel Superalloy, Heat Treatment: 1121°C (2050°F) + Age Data provided by Allvac.Applications: Land based gas turbine blades. |