Titanium 6-2-4-2-.1 is stocked by 2 North American distributors and produced by 6 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 Bar Products by 1 distributors but is also available to a lesser extent in Flat Rolled Products, and Wire Products.
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For mill (large volume) production click here
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Specifications
The following specifications cover Titanium 6-2-4-2-.1
Property Results
Chemistry Data : [top]
Aluminum
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5.5 - 6.5 |
Carbon
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0.08 max |
Hydrogen
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0.0125 max |
Iron
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0.25 max |
Molybdenum
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1.75 - 2.25 |
Nitrogen
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0.05 max |
Oxygen
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0.12 max |
Silicon
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0.1 max |
Tin
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1.75 - 2.25 |
Titanium
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Balance |
Zirconium
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3.5 - 4.5 |
Principal Design Features
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This near beta alloy is generally intended for high temperature use in environments up to 538 C(1000 F).It is only available at the producer level in bar, billet, sheet and plate. Beta Transus (F +/- 25) 1820.
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Applications
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Typical applications include "hot section" gas turbine components such as discs, impellers, turbines, etc. It is also employed in a variety of sheet metal components such as afterburner cans and hot airframe 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 can be hot or cold formed and will exhibit characteristics equivalent to those found in a 1/8 to 1/4 hard austenitic stainless steel.
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Welding
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Rated as "fair in terms of weldability.
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Heat Treatment
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Solution treat at beta minus 14 C(25 F).
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Forging
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Rough forge at 1038-1066 C(1930-1980 F), finish at 954-982 C(1770-1825 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 alloy are similar to those found in 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 recommended to reattain maximum performance characteristics.
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Annealing
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Duplex anneal at 900 C(1670 F) for 1/2 hour, air cool to 788 C(1465 F) for 1/4 hour, air cool. Beta anneal at 1024 C(1900 F) for 1/2-1 hour, air cool to 593 C(1100 F), hold for 8 hours and air cool.
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Aging
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Hold at 538-593 C(1000-1100 F) for 8 hours, air cool.
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Other Physical Props
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Beta Transus (F +/- 25) 1820
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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 Gravity
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4.54
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Electrical Resistivity (microhm-cm (at 68 Deg F))
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191
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Melting Point (Deg F)
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3100
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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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25
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Mechanical Data : [top]
Form |
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Sheet |
Condition |
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Test Specimen Annealed |
Temper |
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70 |
Tensile Strength |
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130 |
Yield Strength |
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120 |
Elongation |
|
10 |
Reduction of Area |
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25 |
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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 |
|
95 |
Yield Strength |
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75 |
Elongation |
|
15 |
Reduction of Area |
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40 |
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Form |
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Sheet |
Condition |
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Test Specimen Annealed |
Temper |
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800 |
Tensile Strength |
|
85 |
Yield Strength |
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70 |
Elongation |
|
20 |
Reduction of Area |
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55 |
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Form |
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Sheet |
Condition |
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Test Specimen Annealed |
Temper |
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1000 |
Tensile Strength |
|
75 |
Yield Strength |
|
60 |
Elongation |
|
25 |
Reduction of Area |
|
65 |
Videos :
MSO currently has no videos available for this grade.
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Disclaimer
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