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Ti6Al2Sn4Zr2Mo Ti Alloy

Description

Ti6Al2Sn4Zr2Mo Ti Alloy Ti Alloy and Mechanical Properties, Chemical Element, Cross Reference, Datasheet.

Datasheet for: Steel Grades:Ti Alloy: Ti6Al2Sn4Zr2Mo Ti Alloy

Chemical composition(mass fraction)(wt.%) of the Ti6Al2Sn4Zr2Mo Ti Alloy

 

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Ti6Al2Sn4Zr2Mo Ti Alloy

Our advantages

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.

We serve you with our honesty, integrity, and professionality.


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 %

 

Users viewing this material also viewed the following:
Titanium Ti-6Al-2Sn-4Zr-2Mo (Ti-6-2-4-2), Sheet
Titanium Ti-6Al-2Sn-4Zr-2Mo-0.1Si; Duplex Annealed
Allvac® 6-2-4-2 Titanium Alloy, Heat Treatment: 982°C (1800°F) + Age
Titanium Ti-6Al-4V (Grade 5), Annealed
Titanium Ti-6Al-2Nb-1Ta-0.8Mo (Ti-621/0.8), Alpha-Annealed

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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Mechanical Properties of steel grade Ti6Al2Sn4Zr2Mo Ti Alloy

Yield
Rp0.2 (MPa)
Tensile
Rm (MPa)
Impact
KV/Ku (J)
Elongation
A (%)
Reduction in cross section on fracture
Z (%)
As-Heat-Treated Condition Brinell hardness (HBW)
131 (≥) 762 (≥) 42 12 14 Solution and Aging, Annealing, Ausaging, Q+T,etc 414

Physical Properties of steel grade Ti6Al2Sn4Zr2Mo Ti Alloy

Temperature
(°C)
Modulus of elasticity
(GPa)
Mean coefficient of thermal expansion 10-6/(°C) between 20(°C) and Thermal conductivity
(W/m·°C)
Specific thermal capacity
(J/kg·°C)
Specific electrical resistivity
(Ω mm²/m)
Density
(kg/dm³)
Poisson’s coefficient, ν
14 - -     0.12 -  
171 914 - 41.3 212   -  
737 - 13 42.2   323 234

Heat Treatment of steel grade Ti6Al2Sn4Zr2Mo Ti Alloy

Heat treated : 1833°C - 1722°C

Technological Curves of steel grade Ti6Al2Sn4Zr2Mo Ti Alloy

Cross Reference Table (Equivalent Grade) of Ti6Al2Sn4Zr2Mo Ti Alloy

Grade Standard Country Application
Q195 China Engineering and welding
Q215 China Engineering and welding
Q215 B China Engineering and welding
Q235 China Engineering and welding
Q235 B China Engineering and welding
Q235 C China Engineering and welding
Q235 D China Engineering and welding
Q255 A China Engineering and welding
Q255 B China Engineering and welding
Q275 China Engineering and welding
Q235q C China Bridge structure with steel
Q235q D China Bridge structure with steel
Q345q E China Bridge structure with steel
Q345q C China Bridge structure with steel
ASTM 1030 ASTM USA General use carbon steel bar
UNS G10300 UNS USA General use carbon steel bar
ASTM 1005 ASTM USA General use carbon steel bar
UNS G10050 UNS USA General use carbon steel bar
ASTM 1006 ASTM USA General use carbon steel bar
UNS G10060 UNS USA General use carbon steel bar

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