The following specifications cover Titanium CP Grade 12
- ASTM B265 (12)
- ASTM B337 (12)
- ASTM B338 (12)
- ASTM B348 (12)
- ASTM B381 (F-12)
- UNS R53400
- Commercially Pure Grade 12
Carbon | 0.08 max | |
Hydrogen | 0.015 max | |
Iron | 0.3 max | |
Molybdenum | 0.2 – 0.4 | |
Nickel | 0.6 – 0.9 | |
Nitrogen | 0.03 max | |
Oxygen | 0.25 max | |
Titanium | Balance |
Principal Design Features | This near-alpha alloy combines excellent strength at high temperatures with excellent weldability and crevice corrosion resistance. Beta Transus (F +/- 25) 1634. | |
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Applications | Generally employed in elevated temperature chemical manufacturing equipment where crevice corrosion is a concern. Also applied to a variety of marine and airframe components. | |
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Machinability | 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 | 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 | Rated as “excellent” in terms of weldability. | |
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Heat Treatment | Not hardenable by heat treatment. | |
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Forging | Rough work at 871 C (1600 F), finish at 788-843 C (1450-1550 F) | |
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Hot Working | 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 | 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 | Heat to 732-816 C (1350- 1500 F),hold for 2 hours follow by air cooling. For intermediate stress relieving, heat to 538-649 C(1000-1200 F) and hold for 1 hour followed by air cooling. | |
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Other Physical Props | Beta Transus (F +/- 25) 1634 | |
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Density (lb / cu. in.) | 0.163 |
Specific Heat (Btu/lb/Deg F – [32-212 Deg F]) | 0.13 |
Electrical Resistivity (microhm-cm (at 68 Deg F)) | 52 |
Melting Point (Deg F) | 3020 |
Thermal Conductivity | 11 |
Modulus of Elasticity Tension | 15 |
Reduction of Area | 25 |
Form | Sheet | ||
Condition | Test Specimen Annealed | ||
Temper | 70 | ||
Tensile Strength | 70 | ||
Yield Strength | 50 | ||
Elongation | 18 | ||
Reduction of Area | 25 |
Limitation of Liability and Disclaimer of Warranty: In no event will South Coast Industrial Metals or any of its affiliates be liable for any damages arising from the use of the information included in this document or that it is suitable for the ‘applications’ noted. We believe the information and data provided to be accurate to the best of our knowledge but, all data is considered typical values only. It is intended for reference and general information and not recommended for specification, design or engineering purposes. South Coast Industrial Metals, Inc. assumes no implied or express warranty in regard to the creation or accuracy of the data provided in this document.