Titanium 5-2.5 is stocked by 7 North American distributors and produced by 8 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 Wire Products by 4 distributors but is also available to a lesser extent in Forging Products, Bar Products, and Flat Rolled Products.
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Specifications
The following specifications cover Titanium 5-2.5
- AMS 4910
- AMS 4926
- AMS 4966
- ASTM B265
- ASTM B348
- ASTM B381
- MIL F-83142
- MIL T-81556
- MIL T-81915
- MIL T-9046
- MIL T-9047
- UNS R54520
Property Results
Related Metals:
- RMI 5Al-2.5Sn(tm)
- 5Al-2.5Sn
Chemistry Data : [top]
Aluminum
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4 - 6 |
Carbon
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0.08 max |
Hydrogen 2
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0.02 max |
Iron
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0.5 max |
Nitrogen
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0.05 max |
Oxygen 2
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0.2 max |
Tin
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2 - 3 |
Titanium
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Balance |
Principal Design Features
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This non-heat treatable, alpha alloy combines good weldability with stability and excellent strength from cryogenic through elevated temperatures. It is available at the mill level in sheet, strip, plate, bar, billet, extrusions and wire. Beta Transus (F +/- 25) 1900.
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Applications
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Primarily employed in aircraft engine and airframe applications.
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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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May be hot or cold formed using hydropress, power brake, stretch or drop hammer methods. Similar in characteristics to 300 series stainless steels.
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Welding
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Rated as "good" in terms of weldability.
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Heat Treatment
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This alloy is not hardenable by heat treatment.
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Forging
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Rough work at 1010-1038 C(1850-1900 F) and finish at 954-1010 C(1750-1850 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 work characteristics of this material is similar to that of a moderately tempered austenitic stainless steel. In multiple cold forming operations, intermediate stress relief is recommended to prevent tearing or other material damage. Post-work annealing is required to reattain optimum performance characteristics.
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Annealing
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For full anneal, heat to 718-843 C(1325-1550 F) 4 hours, air cool. For intermediate stress relieving, heat to 538-650 C(1000-1200 F) for 1 hour, air cool.
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Other Physical Props
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Beta Transus (F +/- 25) 1900
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Physical Data : [top]
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Density (lb / cu. in.)
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0.162
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Specific Heat (Btu/lb/Deg F - [32-212 Deg F])
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0.125
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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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2910
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Thermal Conductivity
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4.5
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Modulus of Elasticity Tension
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16
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Reduction of Area
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25
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Mechanical Data : [top]
MSO currently has no data available for this grade.
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Videos :
MSO currently has no videos available for this grade.
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Disclaimer
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