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Ti6Al2Sn4Zr2Mo

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Ti6Al2Sn4Zr2Mo properties and heat treatment forged piece, Including Ti6Al2Sn4Zr2Mo application and specifications, We have all specifications,Including Ti6Al2Sn4Zr2Mo steel plate, Ti6Al2Sn4Zr2Mo sheet, Ti6Al2Sn4Zr2Mo square steel, Ti6Al2Sn4Zr2Mo flat bar,Ti6Al2Sn4Zr2Mo round bar,Ti6Al2Sn4Zr2Mo forgings, we can own production and sales.


Introduction to Our Products:

Specialized high quality steel

We have the advantages of equipment, technologies and price

forged/hot rolling/ extrusion of steel


We can produce the Ti6Al2Sn4Zr2Mo 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.

Ultrasonic inspection: 100% ultrasonic inspection for any inperfections or based on the customer's requirementExcellent service for all kinds of industries,with advantages of technologies, equipment and price.

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Chemical composition % of the ladle analysis of grade Ti6Al2Sn4Zr2Mo and Standards

Titanium Ti-6Al-2Sn-4Zr-2Mo (Ti-6-2-4-2), Duplex Annealed
Categories: Metal; Nonferrous Metal; Titanium Alloy; Alpha/Near Alpha Titanium Alloy

Material Notes: Alpha Alloy. Silicon is often added to improve creep resistance (See Ti-6242S).

Applications: High-temp jet engines. Blades, discs, spacers, seals. High performance automotive valves.

1 other Heat Treatment of this alloy is in MatWeb.

Key Words: Ti6Al2Sn4Zr2Mo, Ti-6242; Ti-6-2-4-2; UNS R54620

Physical Properties Metric English Comments
Density  4.54 g/cc 0.164 lb/in³
 
Mechanical Properties Metric English Comments
Hardness, Brinell  304 304 Estimated from Rockwell C.
Hardness, Knoop  330 330 Estimated from Rockwell C.
Hardness, Rockwell C  32 32
Hardness, Vickers  318 318 Estimated from Rockwell C.
Tensile Strength, Ultimate  940 MPa 136000 psi
Tensile Strength, Yield  860 MPa 125000 psi
Elongation at Break  15.0 % 15.0 %
Modulus of Elasticity  113.8 GPa 16510 ksi
Compressive Yield Strength  1070 MPa 155000 psi
Notched Tensile Strength  1170 MPa 170000 psi Kt (stress concentration factor) = 3.0
Ultimate Bearing Strength  2000 MPa 290000 psi e/D = 2
Bearing Yield Strength  1620 MPa 235000 psi e/D = 2
Poissons Ratio  0.320 0.320
Charpy Impact  20.0 J 14.8 ft-lb V-notch
Fatigue Strength  280 MPa
@# of Cycles 1.00e+7
40600 psi
@# of Cycles 1.00e+7
Kt (stress concentration factor) = 3.0
  480 MPa
@# of Cycles 1.00e+7
69600 psi
@# of Cycles 1.00e+7
unnotched
Shear Modulus  43.1 GPa 6250 ksi Calculated
Shear Strength  660 MPa 95700 psi Ultimate shear strength
 
Electrical Properties Metric English Comments
Electrical Resistivity  0.000190 ohm-cm 0.000190 ohm-cm
 
Thermal Properties Metric English Comments
CTE, linear 7.70 µm/m-°C
@Temperature 20.0 - 100 °C
4.28 µin/in-°F
@Temperature 68.0 - 212 °F
  8.10 µm/m-°C
@Temperature 20.0 - 315 °C
4.50 µin/in-°F
@Temperature 68.0 - 599 °F
average
  8.10 µm/m-°C
@Temperature 20.0 - 540 °C
4.50 µin/in-°F
@Temperature 68.0 - 1000 °F
average
Specific Heat Capacity  0.460 J/g-°C 0.110 BTU/lb-°F
Thermal Conductivity  7.10 W/m-K 49.3 BTU-in/hr-ft²-°F
Melting Point  <= 1700 °C <= 3090 °F Liquidus; Estimated from similar materials
Liquidus  1700 °C 3090 °F Estimated from similar materials
Beta Transus  990 °C 1810 °F
 
Component Elements Properties Metric English Comments
Aluminum, Al  6.0 % 6.0 %
Molybdenum, Mo  2.0 % 2.0 %
Tin, Sn  2.0 % 2.0 %
Titanium, Ti  86.0 % 86.0 %
Zirconium, Zr  4.0 % 4.0 %

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MTA641 / 14132
 




Machining performance

Download Ti6Al2Sn4Zr2Mo 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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