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Ensinger PEI

Titanium Ti-6Al-6V-2Sn (Ti-6-6-2) STA 910°C/540°C (1000°F)
Categories: Metal; Nonferrous Metal; Titanium Alloy; Alpha/Beta Titanium Alloy

Material Notes: Information provided by Allvac and the references. Solution Treated 910ºC 1 hour, Aged 540ºC for 6 hours. 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 PropertiesMetricEnglishComments
Density 4.54 g/cc0.164 lb/in³
 
Mechanical PropertiesMetricEnglishComments
Hardness, Brinell 411411Estimated from Rockwell C.
Hardness, Knoop 450450Estimated from Rockwell C.
Hardness, Rockwell C 4444
Hardness, Vickers 430430Estimated from Rockwell C.
Tensile Strength, Ultimate 1280 MPa186000 psi
Tensile Strength, Yield 1210 MPa175000 psi
Elongation at Break 10 %10 %
Tensile Modulus 117 GPa17000 ksi
Compressive Yield Strength 1280 MPa186000 psi
Notched Tensile Strength 690 MPa100000 psiKt (stress concentration factor) = 17
Ultimate Bearing Strength 2240 MPa325000 psie/D = 2
Bearing Yield Strength 1790 MPa260000 psie/D = 2
Poissons Ratio 0.320.32
Fatigue Strength  210 MPa
@# of Cycles 1.00e+7
30500 psi
@# of Cycles 1.00e+7
Kt (stress concentration factor) = 4.0
 690 MPa
@# of Cycles 1.00e+7
100000 psi
@# of Cycles 1.00e+7
Fracture Toughness 24.0 MPa-m½21.8 ksi-in½KIC
Shear Modulus 45.0 GPa6530 ksi
Shear Strength 760 MPa110000 psiUltimate shear strength
Charpy Impact 9.50 J7.01 ft-lbV-notch
 
Electrical PropertiesMetricEnglishComments
Electrical Resistivity 0.000157 ohm-cm0.000157 ohm-cm
Magnetic Permeability 1.01.0non-magnetic
 
Thermal PropertiesMetricEnglishComments
CTE, linear  8.60 µm/m-°C
@Temperature 20.0 - 100 °C
4.78 µin/in-°F
@Temperature 68.0 - 212 °F
 9.40 µm/m-°C
@Temperature 20.0 - 315 °C
5.22 µin/in-°F
@Temperature 68.0 - 599 °F
average
Specific Heat Capacity 0.670 J/g-°C0.160 BTU/lb-°F
 0.687 J/g-°C
@Temperature 260 °C
0.164 BTU/lb-°F
@Temperature 500 °F
 0.712 J/g-°C
@Temperature 480 °C
0.170 BTU/lb-°F
@Temperature 896 °F
Thermal Conductivity 6.60 W/m-K45.8 BTU-in/hr-ft²-°F
 8.12 W/m-K
@Temperature 205 °C
56.4 BTU-in/hr-ft²-°F
@Temperature 401 °F
 11.9 W/m-K
@Temperature 425 °C
82.6 BTU-in/hr-ft²-°F
@Temperature 797 °F
Melting Point 1627 - 1649 °C2961 - 3000 °F
Solidus 1627 °C2961 °F
Liquidus 1649 °C3000 °F
Maximum Service Temperature, Air 315 °C599 °FSubject to Tensile Embrittlement
Beta Transus 945 °C1730 °F
 
Component Elements PropertiesMetricEnglishComments
Aluminum, Al 5.0 - 6.0 %5.0 - 6.0 %
Carbon, C <= 0.050 %<= 0.050 %
Copper, Cu 0.35 - 1.0 %0.35 - 1.0 %
Hydrogen, H <= 0.015 %<= 0.015 %
Iron, Fe 0.35 - 1.0 %0.35 - 1.0 %
Nitrogen, N <= 0.040 %<= 0.040 %
Other, each <= 0.10 %<= 0.10 %
Other, total <= 0.30 %<= 0.30 %
Oxygen, O <= 0.20 %<= 0.20 %
Tin, Sn 1.5 - 2.5 %1.5 - 2.5 %
Titanium, Ti 82.895 - 87.8 %82.895 - 87.8 %As Balance; Elemental Composition per ASTM B265
Vanadium, V 5.0 - 6.0 %5.0 - 6.0 %
 
Descriptive Properties
Crystal StructurebccBeta
 cphAlpha

References for this datasheet.

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