Ti-5Al-2.5Sn Grade 6 Ti Alloy Chemical composition and Mechanical properties
Ti-5Al-2.5Sn Grade 6 Ti Alloy
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Ti-5Al-2.5Sn Grade 6 properties and heat treatment forged piece, Including Ti-5Al-2.5Sn Grade 6 application and specifications, We have all specifications，Including Ti-5Al-2.5Sn Grade 6 steel plate, Ti-5Al-2.5Sn Grade 6 sheet, Ti-5Al-2.5Sn Grade 6 square steel, Ti-5Al-2.5Sn Grade 6 flat bar,Ti-5Al-2.5Sn Grade 6 round bar,Ti-5Al-2.5Sn Grade 6 forgings, we can own production and sales.
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We can produce the Ti-5Al-2.5Sn Grade 6 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-5Al-2.5Sn Grade 6 and Standards
Titanium Ti-5Al-2.5Sn (Grade 6)
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: UNS R54520; Ti-5-2.5
| Physical Properties | Metric | English | Comments |
|---|---|---|---|
| Density | 4.48 g/cc | 0.162 lb/in³ | |
| Mechanical Properties | Metric | English | Comments |
| Hardness, Brinell | 320 | 320 | |
| Hardness, Knoop | 363 | 363 | Estimated from Rockwell C. |
| Hardness, Rockwell C | 36 | 36 | |
| Hardness, Vickers | 349 | 349 | Estimated from Rockwell C. |
| Tensile Strength, Ultimate | 861 MPa | 125000 psi | |
| Tensile Strength, Yield | 827 MPa | 120000 psi | |
| Elongation at Break | 15.0 % | 15.0 % | |
| Modulus of Elasticity | 110 - 125 GPa | 16000 - 18100 ksi | |
| Compressive Yield Strength | 830 MPa | 120000 psi | |
| Notched Tensile Strength | 1240 MPa | 180000 psi | Kt (stress concentration factor) = 6.5 |
| Ultimate Bearing Strength | 1760 MPa | 255000 psi | e/D = 2 |
| Bearing Yield Strength | 1340 MPa | 194000 psi | e/D = 2 |
| Poissons Ratio | 0.310 | 0.310 | Typical for alpha titanium alloy. |
| Charpy Impact | 24.0 J | 17.7 ft-lb | V-notch |
| Fatigue Strength |
290 MPa @# of Cycles 1.00e+7 |
42100 psi @# of Cycles 1.00e+7 |
Kt (stress concentration factor) = 2.4 |
|
380 MPa @# of Cycles 1.00e+7 |
55100 psi @# of Cycles 1.00e+7 |
unnotched | |
|
390 MPa @# of Cycles 100000 |
56600 psi @# of Cycles 100000 |
Kt (stress concentration factor) = 2.4 | |
|
440 MPa @# of Cycles 1.00e+6 |
63800 psi @# of Cycles 1.00e+6 |
unnotched | |
|
530 MPa @# of Cycles 100000 |
76900 psi @# of Cycles 100000 |
Unnotched | |
| Fracture Toughness | 33.0 MPa-m½ | 30.0 ksi-in½ | K(ISCC) |
| 96.0 MPa-m½ | 87.4 ksi-in½ | K(IC) | |
| Shear Modulus | 48.0 GPa | 6960 ksi | |
| Shear Strength | 520 MPa | 75400 psi | Ultimate shear strength |
| Electrical Properties | Metric | English | Comments |
| Electrical Resistivity | 0.000160 ohm-cm | 0.000160 ohm-cm | |
| Thermal Properties | Metric | English | Comments |
| CTE, linear |
9.40 µm/m-°C @Temperature 0.000 - 100 °C |
5.22 µin/in-°F @Temperature 32.0 - 212 °F |
|
|
9.50 µm/m-°C @Temperature 0.000 - 315 °C |
5.28 µin/in-°F @Temperature 32.0 - 599 °F |
average; unspecified heat treatment. | |
|
9.70 µm/m-°C @Temperature 0.000 - 650 °C |
5.39 µin/in-°F @Temperature 32.0 - 1200 °F |
average | |
| Specific Heat Capacity | 0.530 J/g-°C | 0.127 BTU/lb-°F | 0.674 J/g-ºC at 315ºC |
| Thermal Conductivity | 7.80 W/m-K | 54.1 BTU-in/hr-ft²-°F | 10.9 W/m-ºC at 315ºC |
| Melting Point | <= 1590 °C | <= 2890 °F | Liquidus |
| Liquidus | 1590 °C | 2890 °F | |
| Beta Transus | 1040 - 1090 °C | 1900 - 1990 °F | |
| Component Elements Properties | Metric | English | Comments |
| Aluminum, Al | 4.00 - 6.00 % | 4.00 - 6.00 % | |
| Carbon, C | <= 0.100 % | <= 0.100 % | |
| Hydrogen, H | <= 0.0150 % | <= 0.0150 % | |
| Iron, Fe | <= 0.500 % | <= 0.500 % | |
| Nitrogen, N | <= 0.0300 % | <= 0.0300 % | |
| Other, each | <= 0.0500 % | <= 0.0500 % | |
| Other, total | <= 0.300 % | <= 0.300 % | |
| Oxygen, O | <= 0.200 % | <= 0.200 % | |
| Tin, Sn | 2.00 - 3.00 % | 2.00 - 3.00 % | |
| Titanium, Ti | 89.855 - 94.0 % | 89.855 - 94.0 % | As Balance; Elemental Compostions per ASTM B265 |
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Machining performance
Download Ti-5Al-2.5Sn Grade 6 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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