UNS R56210 Ti Alloy

UNS R56210 Ti Alloy

Our advantages

UNS R56210 properties and heat treatment forged piece, Including UNS R56210 application and specifications, Including UNS R56210 tube plate, UNS R56210 Pipe Fitting, UNS R56210 flange, UNS R56210 Angle Bar,UNS R56210 Valve,UNS R56210 3d bend.

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Introduction to Our Products:

Specialized high quality steel

We have the advantages of equipment, technologies and price

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UNS R56210 has the following specifications:

Valve:
Diameter : 1mm-1300mm

Steel pipe:
Size: OD: 9.5mm - 813mm WT: 0.8mm - 34mm Length: 1 - 13m, also can be customed.

Pipe fitting:
Size: 1/8 inch - 80 inch (DN6 - DN2000) WT: Sch5s - Sch160XXS

Flange:

Length:  Any length based on the customer's requirement.

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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 %

Users viewing this material also viewed the following:
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Titanium Ti-6Al-2Sn-4Zr-2Mo-0.1Si; Duplex Annealed
Titanium Ti-8Al-1Mo-1V (Ti-8-1-1)
Titanium Ti-6Al-2Nb-1Ta-1Mo, Annealed
Titanium Ti-6Al-2Nb-1Ta-0.8Mo (Ti-621/0.8), as-rolled

MTA611 / 14130

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Machining performance

UNS R56210 the mechanical properties of the report, the report provides detailed performance analysis and application.

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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.

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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.

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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.

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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.

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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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