Ti-6Al-2Sn-1.5Zr-1Mo-0.35Bi-0.1Si Ti Alloy Chemical composition and Mechanical properties
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Ti-6Al-2Sn-1.5Zr-1Mo-0.35Bi-0.1Si Ti Alloy
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Ti-6Al-2Sn-1.5Zr-1Mo-0.35Bi-0.1Si properties and heat treatment forged piece, Including Ti-6Al-2Sn-1.5Zr-1Mo-0.35Bi-0.1Si application and specifications, We have all specifications，Including Ti-6Al-2Sn-1.5Zr-1Mo-0.35Bi-0.1Si steel plate, Ti-6Al-2Sn-1.5Zr-1Mo-0.35Bi-0.1Si sheet, Ti-6Al-2Sn-1.5Zr-1Mo-0.35Bi-0.1Si square steel, Ti-6Al-2Sn-1.5Zr-1Mo-0.35Bi-0.1Si flat bar,Ti-6Al-2Sn-1.5Zr-1Mo-0.35Bi-0.1Si round bar,Ti-6Al-2Sn-1.5Zr-1Mo-0.35Bi-0.1Si forgings, we can own production and sales.
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We can produce the Ti-6Al-2Sn-1.5Zr-1Mo-0.35Bi-0.1Si 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 Ti-6Al-2Sn-1.5Zr-1Mo-0.35Bi-0.1Si and Standards
Titanium 11 (Ti-6Al-2Sn-1.5Zr-1Mo-0.35Bi-0.1Si)
Categories: Metal; Nonferrous Metal; Titanium Alloy; Alpha/Near Alpha Titanium Alloy
Material Notes: 1 other heat treatment of this alloy is in MatWeb.
| Physical Properties | Metric | English | Comments |
|---|---|---|---|
| Density | 4.50 g/cc | 0.163 lb/in³ | |
| Mechanical Properties | Metric | English | Comments |
| Tensile Strength, Ultimate | 1030 MPa | 149000 psi | |
| Tensile Strength, Yield | 930 MPa | 135000 psi | |
| Elongation at Break | 16.0 % | 16.0 % | |
| Reduction of Area | 34.0 % | 34.0 % | |
| Modulus of Elasticity | 115 GPa | 16700 ksi | Typical value for an alpha titanium alloy |
| Poissons Ratio | 0.310 | 0.310 | Typical for alpha titanium alloy. |
| Shear Modulus | 43.9 GPa | 6370 ksi | Calculated from typical values. |
| Electrical Properties | Metric | English | Comments |
| Electrical Resistivity | 0.000160 ohm-cm | 0.000160 ohm-cm | Estimated from similar alpha titanium alloys. |
| Thermal Properties | Metric | English | Comments |
| CTE, linear |
9.00 µm/m-°C @Temperature 20.0 - 100 °C |
5.00 µin/in-°F @Temperature 68.0 - 212 °F |
Typical alpha titanium alloy |
| Specific Heat Capacity | 0.525 J/g-°C | 0.125 BTU/lb-°F | Typical value for titanium alloys. |
| Thermal Conductivity | 7.00 W/m-K | 48.6 BTU-in/hr-ft²-°F | Estimated from similar titanium alloys. |
| Beta Transus | 980 - 1015 °C | 1800 - 1859 °F | |
| Component Elements Properties | Metric | English | Comments |
| Aluminum, Al | 6.0 % | 6.0 % | |
| Bismuth, Bi | 0.35 % | 0.35 % | |
| Molybdenum, Mo | 1.0 % | 1.0 % | |
| Silicon, Si | 0.10 % | 0.10 % | |
| Tin, Sn | 2.50 % | 2.50 % | |
| Titanium, Ti | 89.0 % | 89.0 % | |
| Zirconium, Zr | 1.50 % | 1.50 % | |
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Machining performance
Download Ti-6Al-2Sn-1.5Zr-1Mo-0.35Bi-0.1Si 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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