UNS R56210 Ti Alloy Chemical composition and Mechanical properties
UNS R56210 Ti Alloy
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UNS R56210 properties and heat treatment forged piece, Including UNS R56210 application and specifications, We have all specifications，Including UNS R56210 steel plate, UNS R56210 sheet, UNS R56210 square steel, UNS R56210 flat bar,UNS R56210 round bar,UNS R56210 forgings, we can own production and sales.
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We can produce the UNS R56210 has the following specifications:
Round bar steel: 1mm to 3000mm
Square-shape steel: 1mm to 2000mm
Plate steel:0.1mm to 2500mm
Width: 10mm to 2500mm
Lenth: We can supply any lenth based on the customer's requirement.
Forging: Shafts with flanks/pipes/tubes/slugs/donuts/cubes/other shapes
Tubings: OD: φ6-219 mm, with wall thickness ranging from 1-35 mm.
Finished goods condition: hot forging/hot rolling + annealing/normalizing + tempering/quenching + tempering/any conditions based on the customer's requirement
Surface conditions: scaled (hot working finish)/ground/rough machining/fine machining/based on the customer's requirement
Furnaces for metallurgical processing: electrode arc + LF/VD/VOD/ESR/Vacuum consumable electrode.
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Chemical composition % of the ladle analysis of grade UNS R56210 and Standards
Titanium Ti-6Al-2Nb-1Ta-1Mo
Categories: Metal; Nonferrous Metal; Titanium Alloy; Alpha/Near Alpha Titanium Alloy
Material Notes: 1 other heat treatment of this alloy is in MatWeb.
Key Words: Ti6Al2Nb1Ta1Mo, Ti-6211; Ti-621/0.8; UNS R56210
| Physical Properties | Metric | English | Comments |
|---|---|---|---|
| Density | 4.48 g/cc | 0.162 lb/in³ | |
| Mechanical Properties | Metric | English | Comments |
| Hardness, Brinell | 290 | 290 | Estimated from Rockwell C. |
| Hardness, Knoop | 315 | 315 | Estimated from Rockwell C. |
| Hardness, Rockwell C | 30 | 30 | |
| Hardness, Vickers | 304 | 304 | Estimated from Rockwell C. |
| Tensile Strength, Ultimate | 830 MPa | 120000 psi | |
| Tensile Strength, Yield | 730 MPa | 106000 psi | |
| Elongation at Break | 13.0 % | 13.0 % | |
| Modulus of Elasticity | 113.8 GPa | 16510 ksi | |
| Poissons Ratio | 0.310 | 0.310 | Typical for alpha titanium alloy. |
| Charpy Impact | 31.0 J | 22.9 ft-lb | V-notch |
| Shear Modulus | 43.4 GPa | 6290 ksi | Calculated from typical values. |
| Electrical Properties | Metric | English | Comments |
| Electrical Resistivity | 0.000154 ohm-cm | 0.000154 ohm-cm | Annealed |
| Thermal Properties | Metric | English | Comments |
| CTE, linear |
9.00 µm/m-°C @Temperature 20.0 - 615 °C |
5.00 µin/in-°F @Temperature 68.0 - 1140 °F |
average |
|
9.20 µm/m-°C @Temperature 20.0 - 93.0 °C |
5.11 µin/in-°F @Temperature 68.0 - 199 °F |
annealed | |
| Specific Heat Capacity | 0.550 J/g-°C | 0.131 BTU/lb-°F | Estimated from similar materials |
| Thermal Conductivity | 6.40 W/m-K | 44.4 BTU-in/hr-ft²-°F | |
| Melting Point | <= 1650 °C | <= 3000 °F | Liquidus; Estimated from similar materials |
| Liquidus | 1650 °C | 3000 °F | Estimated from similar materials |
| Beta Transus | 1016 °C | 1861 °F | |
| Component Elements Properties | Metric | English | Comments |
| Aluminum, Al | 6.0 % | 6.0 % | |
| Molybdenum, Mo | 1.0 % | 1.0 % | |
| Niobium, Nb (Columbium, Cb) | 2.0 % | 2.0 % | |
| Tantalum, Ta | 1.0 % | 1.0 % | |
| Titanium, Ti | 90.0 % | 90.0 % | |
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MTA611 / 14130
Machining performance
Download UNS R56210 the mechanical properties of the report, the report provides detailed performance analysis and application. Download >>
Principal Design Features
One of the most widely used precipitation hardening grades in the business. While soft and ductile in the solution annealed condition, it is capable of high properties with a single precipitation or aging treatment. Characterized by good corrosion resistance, high harness, toughness and strength.
Machinability
Long, gummy chips characterize this alloys machinability. It can be machined in the annealed condition, however condition H1150M will yield best results. Post machining solution treatment of parts will be required prior to final hardening if machining in this condition.
Heat Treatment
CONDITION A--Soak at 1900 F (1038 C) for 30 minutes and cool below 60 F (16 C) for complete martensite transformation. CONDITION H 950- Treat Condition A material at 900 F(482 C) for 1 hour, air cool.. CONDITION H925, H1025, H1075, H1100, H1150- Soak solution treated material for 4 hours at specified temperature, air cool, CONDITION H1150M- Soak solution treated material at 1400 F (760 C) for 2 hours, air cool, then re-heat to 1150 F (620 C) for 4 hours and air cool.
Welding
Successfully welded by common fusion and resistance methods, this alloy should not be joined by oxyacetylene welding. AWS E/ER630 filler metal is recommended if required.
Forging
Soak for 1 hour at 2150 F (1177 C) prior to forging. Do not work below 1850 F (1010 C). Post-work solution treatment is required prior to final hardening.
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