Titanium 6-6-2 is stocked by 6 North American distributors and produced by 14 large mills. Distributors will offer small quantity buys while mills will generally only sell large quantities, with delivery times anywhere from 10 to 50 weeks depending on size and form required
This material is stocked primarily in Flat Rolled Products by 5 distributors but is also available to a lesser extent in Bar Products, Wire Products, Fasteners, Forging Products, Shapes, and Tubular Products.
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Specifications
The following specifications cover Titanium 6-6-2
- AMS 4918
- AMS 4936
- AMS 4971
- AMS 4978
- AMS 4979
- DMS 1870
- DMS 1887
- MIL F-83142
- MIL T-81556
- MIL T-9046
- MIL T-9047
- UNS R56620
Property Results
Related Metals:
- 6Al-6V-2Sn
- Allvac 6-6-2(tm)
- RMI 6Al-6V-2Sn(tm)
Chemistry Data : [top]
Aluminum
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5 - 6 |
Carbon
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0.05 max |
Copper
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0.35 - 1 |
Hydrogen 2
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0.015 max |
Iron
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0.35 - 1 |
Nitrogen
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0.04 max |
Oxygen
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0.2 max |
Tin
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1.5 - 2.5 |
Titanium
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Balance |
Vanadium
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5 - 6 |
Principal Design Features
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This alpha-beta alloy can be heat treated to higher strengths and heavier section sizes than alloy 6AL-4V. It combines excellent strength, corrosion resistance and moderately good fabricability. Beta Transus (F +/- 25) 1735.
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Applications
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Used primarily in plate and forging applications for airframe sections, rocket cases and ordnance components.
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Machinability
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As a family, titanium and its alloys have developed a mystique as a nightmare to machine. This is simply not the case. Experienced operators have compared its characteristics to those found in 316 stainless steel. Recommended practice includes high coolant flow(to offset the material's low thermal conductivity), slow speeds and relatively high feed rates. Tooling should be tungsten carbide designations C1-C4 or cobalt type high speed tools.
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Forming
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This alloy may be hot or cold formed. Popular methods include hydropress, stretch or drop-hammer. This material responds similarly to 300 series stainless steels.
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Welding
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Beta Transus (F +/- 25) 1735
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Heat Treatment
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Solution treat at 843-913 C(1550-1675 F) for 1 hour and water cool.
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Forging
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Rough at 932 C(1710 F), finish at 843 C(1550 F).
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Hot Working
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Hot forming will reduce both the springback and required forming forces, and will increase the overall ductility of the material.
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Cold Working
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The cold working characteristics of this material are similar to those of austenitic stainless steels. In multiple forming operations, intermediate stress relieving is recommended to offset the alloy's tendency to work harden. Post-work annealing is required to re-attain optimum performance characteristics.
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Annealing
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Hold at 704 C(1300 F) for 2 hours, air cool. For stress relieving, hold at 593 C(1100 F) for 2 hours and air cool.
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Aging
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Age at 538-621 C(1000-1150 F) for 4-8 hours and air cool.
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Other Physical Props
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Beta Transus (F +/- 25) 1735
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Physical Data : [top]
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Density (lb / cu. in.)
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0.164
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Specific Heat (Btu/lb/Deg F - [32-212 Deg F])
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0.155
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Electrical Resistivity (microhm-cm (at 68 Deg F))
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157
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Melting Point (Deg F)
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3100
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Thermal Conductivity
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4.2
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Modulus of Elasticity Tension
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16.5
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Reduction of Area
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20
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Mechanical Data : [top]
Form |
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Sheet |
Condition |
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Solution Annealed & Aged |
Temper |
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70 |
Tensile Strength |
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150 |
Yield Strength |
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140 |
Elongation |
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10 |
Reduction of Area |
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20 |
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Form |
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Sheet |
Condition |
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Test Specimen Annealed |
Temper |
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70 |
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Form |
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Sheet |
Condition |
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Test Specimen Annealed |
Temper |
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400 |
Tensile Strength |
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145 |
Yield Strength |
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127 |
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Form |
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Sheet |
Condition |
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Test Specimen Annealed |
Temper |
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600 |
Tensile Strength |
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135 |
Yield Strength |
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117 |
Videos :
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