AMS4965 Ti6Al4V Titanium Alloy Bars, Forgings and Rings

  • Grade: Ti6Al4V, Grade 5
  • Annealed condition
  • Bar, Rings, Forgings
  • High Strength and Fatigue Resistance
  • Good Corrosion Resistance
  • Lightweight
  • Good Biocompatibility
  • Heat Treatability

Features

AMS4965 Ti6Al4V Titanium Alloy Bars, Forgings and Rings Solution Heat Treated and Aged

AMS4965 Ti6Al4V Chemical Composition (wt.%) of AMS4965 Ti6Al4V Titanium Alloy Bars, Forgings and Rings

Element Min Max
Aluminum 5.50 6.75
Vanadium 3.50 4.50
Iron 0.30
Oxygen 0.20
Carbon 0.08
Nitrogen 0.05 (500 ppm)
Hydrogen (3.1.1) 0.0125 (125 ppm)
Yttrium (3.1.2) 0.005 (50 ppm)
Residual Elements, each (3.1.2) 0.10
Residual Elements, total (3.1.2) 0.40
Titanium remainder

Mechanical Properties (Minimum) of AMS4965 Ti6Al4V Titanium Alloy Bars, Forgings and Rings

Nominal Diameter or Distance Between Parallel Sides (mm) Tensile Strength (MPa) Yield Strength at 0.2% Offset (MPa) Elongation (1) in 50.8 mm or 4D (%) (L) Elongation (1) in 50.8 mm or 4D (%) (T) Reduction of Area (%) (L)
Up to 12.70, incl 1138 1069 10 20
Over 12.70 to 25.40, incl 1103 1034 10 20
Over 25.40 to 38.10, incl 1069 1000 10 20
Over 38.10 to 50.80, incl 1034 965 10 8 20
Over 50.80 to 76.20, incl 965 896 10 8 20
Over 76.20 to 101.60, incl 896 827 8 6 20

Notes:

For forgings, elongation shall be not lower than 8% (L) and 6% (T) for all sizes.

Nominal Thickness Nominal Width Tensile Strength Yield Strength Offset Elongation in L % Elongation in T % Reduction of Area %
Up to 12.70, incl Over 12.70 to 203.20, incl 1103 MPa 1034 MPa 10 10 25
Over 12.70 to 25.40, incl Over 25.40 to 101.60, incl 1069 MPa 1000 MPa 10 10 20
Over 25.40 to 38.10, incl Over 101.60 to 203.20, incl 1034 MPa 965 MPa 10 10 20
Over 38.10 to 50.80, incl Over 38.10 to 101.60, incl 1034 MPa 965 MPa 10 10 20
Over 50.80 to 76.20, incl Over 101.60 to 203.20, incl 1000 MPa 931 MPa 10 10 20
Over 76.20 to 101.60, incl Over 50.80 to 101.60, incl 1000 MPa 931 MPa 10 10 20
Over 101.60 to 203.20, incl Over 76.20 to 203.20, incl 965 MPa 896 MPa 10 10 20

Technical Specifications

Specification Value
Standard AMS4965 Ti6Al4V Titanium Alloy Bars, Wire, Forgings, and Rings Solution Heat Treated and Aged
Grade Ti6Al4V, Grade 5
Type Bar, Wire, Forgings, Rings
Dimension Bar Dia: 0.25 to 12 inches (6.35 to 304.8 mm), Length up to 20 feet (6096 mm)
Wire Dia: 0.020 to 0.500 inches (0.51 to 12.7 mm)
Block: Width: 2 – 24 inches (50 -610mm) x Height: 2 – 24 inches (50-610mm) x Length: 2 – 20 feet (610-6100mm)
Rings: OD: 250-1500mm, ID: 150-1400mm, Height: 20-500mm
Density 4.51g/cm³
Inspection Certificate EN 10204 Type 3.1 (Mill Test Certificate), EN 10204 Type 3.2 (Witness Testing or 3rd Party Inspection)
Tests Chemical Composition, Mechanical Properties
Key Features

High Strength and Fatigue Resistance: Ti-64 exhibits high strength and fatigue resistance, making it suitable for structural components and cyclic loading applications.
Good Corrosion Resistance: It demonstrates good resistance to corrosion in various environments, including seawater, chloride solutions, and some acids.
Lightweight: Ti-64 retains the lightweight characteristic of titanium alloys, contributing to weight savings in components and structures.
Good Biocompatibility: It exhibits good biocompatibility, making it suitable for medical implants and devices.
Heat Treatability: Ti-64 can be heat treated to further enhance its strength and other mechanical properties.

Packing

Packed in plywood boxes.

Applications in Bar Form:

Aircraft structural components: These are used for spars, ribs, fasteners, and other structural parts requiring a high strength-to-weight ratio and fatigue resistance.
Surgical instruments: Employed for scalpels, forceps, and other instruments requiring biocompatibility, strength, and corrosion resistance.
Shafts and fasteners: Utilized for shafts, fasteners, and other components exposed to corrosive chemicals.
High-performance parts: Used for connecting rods, valves, and other parts requiring high strength and low weight.

Applications in Forged Form:

Landing gear components: Forged Ti-64 is used for landing gear components like struts and wheels due to its high strength and fatigue resistance.
Engine mounts and structural parts: Employed for complex shaped components requiring high strength and durability.
Armour plating and structural components: These are used in military vehicles and equipment because they are strong, lightweight, and ballistic resistant.
Joint replacements: Forged Ti-64 is a common material for hip, knee, and other joint replacements due to its strength, wear resistance, and biocompatibility.

Applications in Ring Form:

Jet engine components: These are forged and machined into compressor rings, spacers, and other engine parts requiring high strength and fatigue resistance.
Bearings and seals: These are used for bearing races, seal rings, and other components that need wear and corrosion resistance.

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