Ti-6AL-4V ELI Titanium Bar, Plate - AMS 4930, 6932
Ti-6AL-4V ELI, AMS 4930, is a general purpose alpha-beta alloy. The ELI (extra low interstitials) variant possesses high cycle fatigue strength and is available for fracture critical applications, such as medical implants or aerospace applications. Titanium Grade 23 material is biocompatible, features moderately high tensile strength, improved ductility, good fatigue strength, intermediate fracture toughness, and high resistance to general corrosion in seawater. It is hardenable in sections up to 1" thick.
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Inventory Size Ranges for Ti-6AL-4V ELI
Type | Thickness | AMS Standards | ASTM | Get a Quote |
---|---|---|---|---|
Plate | 0.250" - 1.000" | AMS 4930, AMS 6932 | ASTM B 265 GR 23, ASTM B 348 GR 23, ASTM F 136 | Get a Quote |
Bar | 0.125" - 3.000" | AMS 4930, AMS 6932 | ASTM B 265 GR 23, ASTM B 348 GR 23, ASTM F 136 | Get a Quote |
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Machining Ti-6AL-4V ELI
Our grade of 6AL-4V ELI features consistent machinability. It is stress-relieved, eliminating distortion, and its longitudinal grain flow enhances strength.
We offer the following Ti-6AL-4V products:
Round Bar: Certified to standard 6-4 material AMS 4928. Stocking centerless ground bar (+/- 0.0005”) and precision ground bar (+/- 0.0002”) in sizes from 0.125”– 3.000” for complex CNC/Swiss screw machine applications.
Plate: Comprehensive stock list from multiple U.S. sources. Very tight tolerance on cut piece orders. Ships within 2-3 days. Cut-to-length blanks individually marked with up to 4 lines of information.
Rectangular Bar: Stress-relieved Ti6AL4V ELI stock provides consistent machinability and minimizes distortion. Parallel surfaces ready-to-fit your milling fixtures.
Other industry standards we comply with:
- ASM/MIL-81200
- GE Aircraft Engine (GT193)
Common Trade Names
Industry Applications for Ti-6AL-4V ELI
- Medical Implants and Instrumentation
- Maxillofacial, dental, spinal, trauma, orthopedic and extremities
- Air frames
- Jet and engine rocket components
- Pressure vessels
- Fasteners
- Prosthetic Implants
- Geothermal-well casings
- Automotive components
- Sports equipment
Chemical Composition
Element | Min | Max | |
---|---|---|---|
Ti | Titanium | 88.0 | 91.0 |
Al | Aluminum | 5.5 | 6.5 |
V | Vanadium | 3.5 | 4.5 |
N | Nitrogen | 0.03 | |
C | Carbon | 0.08 | |
O | Oxygen | 0.013 | |
Fe | Iron | 0.25 | |
H | Hydrogen | 0.0125 | |
- | Res. Each | 0.1 | |
- | Res. Total | 0.4 | |
Physical Properties
Physical Property | T (°F) | T (°C) | Value | Value (SI) |
---|---|---|---|---|
Density | 72 | 22 | 0.163 lb in¯³ | 4.42 g cm¯³ |
Beta Transus | 1825±25 | 966±14 | - | - |
Melting (liquidus) Point | 3000-3020±25 | 1650-1660±14 | - | - |
Thermal Conductivity | 68 | 20 | 3.8 Btu hr¯¹°F¯¹ | 6.6 W m¯¹ K¯¹ |
Mil Annealed | 600 | 315 | 6.1 Btu hr¯¹°F¯¹ | 10.6 W m¯¹ K¯¹ |
Specific Heat | 68 | 20 | 0.140 Btu lb¯¹°F¯¹ | 0.580 J g¯¹K¯¹ |
800 | 425 | 0.160 Btu lb¯¹°F¯¹ | 0.670 J g¯¹K¯¹ | |
1600 | 870 | 0.220 Btu lb¯¹°F¯¹ | 0.930 J g¯¹K¯¹ | |
Electrical Resistivity | 32 | 0 | 66 μΩ∙in | 1.68 μΩ∙m |
600 | 315 | 73 μΩ∙in | 1.86 μΩ∙m | |
1200 | 650 | 74μΩ∙in | 1.89 μΩ∙m | |
Magnetic Permeability | 1.00005 at 20 oersteds | |||
Mean Coefficient of Thermal Expansion | 32-212 | 0-100 | 5.0 x 10¯⁶in in ¯¹°F¯¹ | 9.0x10¯⁶⁶m m¯¹°C¯¹ |
70-800 | 20-425 | 5.2 x 10¯⁶in in ¯¹°F¯¹ | 9.4x10¯⁶m m¯¹°C¯¹ | |
70-1200 | 20-650 | 5.4 x 10¯⁶in in ¯¹°F¯¹ | 9.7x10¯⁶m m¯¹°C¯¹ | |
Young's Modulus | 68 | 20 | 15.5-17.7 Msi | 107-122 GPa |
450 | 230 | 13.8-16.2 Msi | 95-111 GPa | |
Shear Modulus | 68 | 20 | 5.9-6.5 Msi | 41-45 GPa |
Poisson's Ratio | 68 | 20 | .31 | .31 |
Mechanical Properties
Product | Condition | Specification | Dir. | Temp, °F (°C) | UTS, ksi (MPa) | .02% YS, ksi (MPa) | %EI | %RA |
---|---|---|---|---|---|---|---|---|
0.025-1.000 Sheet & Plate | St | ASTM B265 | L & LT | 68 (20) | 120 (828) | 110 (759) | 10 | - |
≤3.00 RD or Thk. | Annealed | ASTM B348 | L | 68 (20) | 120 (828) | 110 (759) | 10 | 25 |
≥1.75 RD or Thk. 1.75-2.50 2.50-4.00 | Annealed Annealed Annealed | ASTM F136 ASTM F136 ASTM F136 | L L & LT L, LT & ST | 68 (20) 68 (20) 68 (20) | 120 (828) 120 (860) 120 (825) | 115 (759) 110 (760) 115 (760) | 10 8 8 | 25 20 15 |