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Elmet Technologies

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Titanium Ti-6Al-6V-2Sn (Ti-6-6-2) STA 870°C/565°C
Categories: Metal; Nonferrous Metal; Titanium Alloy; Alpha/Beta Titanium Alloy

Material Notes: Information provided by Allvac and the references. Solution Treated 870ºC, Aged 565ºC. Alpha-Beta alloy.

Characteristics: Good corrosion resistance. Higher strength, lower fracture toughness and lower fatigue properties when compared to Ti-6Al-4V

Applications: Airframes, jet engines, rocket engine cases, nuclear reactor components, ordnance components.

Forms available: Billet, bar, plate, sheet and extrusions.

2 other heat treatments of this alloy are listed in MatWeb.

Key Words: Ti-662; Ti-6-6-2; UNS R56620
Vendors: No vendors are listed for this material. Please click here if you are a supplier and would like information on how to add your listing to this material.
 
Physical PropertiesOriginal ValueComments
Density 4.54 g/cc
 
Mechanical PropertiesOriginal ValueComments
Hardness, Brinell 389Estimated from Rockwell C.
Hardness, Knoop 425Estimated from Rockwell C.
Hardness, Rockwell C 42
Hardness, Vickers 407Estimated from Rockwell C.
Tensile Strength 900 MPa
@Temperature 300 °C
 930 MPa
@Temperature 200 °C
 980 MPa
@Temperature 100 °C
Tensile Strength, Ultimate 1100 MPa
Tensile Strength, Yield 1035 MPa
 760 MPa
@Temperature 300 °C
 820 MPa
@Temperature 200 °C
 880 MPa
@Temperature 100 °C
Elongation at Break 12 %
 15 %
@Temperature 100 °C
 17 %
@Temperature 200 °C
 18 %
@Temperature 300 °C
Reduction of Area 18 %
@Temperature 23.0 °C
 24 %
@Temperature 100 °C
 39 %
@Temperature 200 °C
 42 %
@Temperature 300 °C
Creep Strength 770 MPa
@Temperature 315 °C,
Time >=1.80e+6 sec
strain 0.5%
 800 MPa
@Temperature 315 °C,
Time >=360000 sec
strain 0.5%
 800 MPa
@Temperature 315 °C,
Time >=1.80e+6 sec
strain 1%
 820 MPa
@Temperature 315 °C,
Time >=360000 sec
strain 1%
Modulus of Elasticity 112 GPa
Tensile Modulus 101 GPa
@Temperature 300 °C
 106 GPa
@Temperature 200 °C
 110 GPa
@Temperature 100 °C
Poissons Ratio 0.32
Fatigue Strength 190 MPa
@# of Cycles 1.00e+7
notched
 540 MPa
@# of Cycles 10000
Kt (stress concentration factor) = 3.9
 680 MPa
@# of Cycles 1.00e+7
unnotched sample
 1070 MPa
@# of Cycles 10000
unnotched
Fracture Toughness 60.0 MPa-m½Plane-Strain
 60.0 MPa-m½
@Temperature 22.0 °C
 99.0 MPa-m½
@Temperature 93.0 °C
 143 MPa-m½
@Temperature 205 °C
Shear Modulus 45.0 GPa
 
Electrical PropertiesOriginal ValueComments
Electrical Resistivity 0.000157 ohm-cm
Magnetic Permeability 1.0non-magnetic
 
Thermal PropertiesOriginal ValueComments
CTE, linear 9.00 µm/m-°C
@Temperature 20.0 °C
 9.40 µm/m-°C
@Temperature 20.0 - 315 °C
average
 9.50 µm/m-°C
@Temperature 20.0 - 540 °C
average
Specific Heat Capacity 0.670 J/g-°C
 0.687 J/g-°C
@Temperature 260 °C
 0.712 J/g-°C
@Temperature 480 °C
Thermal Conductivity 6.60 W/m-K
 8.12 W/m-K
@Temperature 205 °C
 11.9 W/m-K
@Temperature 425 °C
Melting Point 1627 - 1649 °C
Solidus 1627 °C
Liquidus 1649 °C
Maximum Service Temperature, Air 315 °CSubject to Tensile Embrittlement
Beta Transus 945 °C
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al 5.0 - 6.0 %
Carbon, C <= 0.050 %
Copper, Cu 0.35 - 1.0 %
Hydrogen, H <= 0.015 %
Iron, Fe 0.35 - 1.0 %
Nitrogen, N <= 0.040 %
Other, each <= 0.10 %
Other, total <= 0.30 %
Oxygen, O <= 0.20 %
Tin, Sn 1.5 - 2.5 %
Titanium, Ti 82.895 - 87.8 %As Balance; Elemental Composition per ASTM B265
Vanadium, V 5.0 - 6.0 %
 
Descriptive Properties
Crystal StructurebccBeta
 cphAlpha

References for this datasheet.

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